A Bianchi Type IV Viscous Model of The Early Universe
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Transcript of A Bianchi Type IV Viscous Model of The Early Universe
A Bianchi Type IV Viscous Model of The Early Universe
Public Lecture August 28, 2012 - 10:00 AM - PSE258
Ikjyot Singh Kohli M.Sc. Candidate
Department of Physics and Astronomy York University
A Bianchi Type IV Viscous Model of The Early Universe
Public Lecture August 28, 2012 - 10:00 AM - PSE258
Ikjyot Singh Kohli M.Sc. Candidate
Department of Physics and Astronomy York University
Quantum Gravity FLRW Metric - Present-Day Model
Early Universe
L = Nph�R+KabK
ab �K2 � 2⇤�
ds2 = �dt2 + a2(t)
dr2
1� kr2+ r2
�d✓2 + sin2 ✓d�2
��
The Early Universe
The Early Universe
We are interested in developing a cosmological model that describes the conditions of the early universe.
The Early Universe
We are interested in developing a cosmological model that describes the conditions of the early universe.
Before we continue, we note that a cosmological model necessarily implies the use of General Relativity
General Relativity: The “Brief” Version!
General Relativity: The “Brief” Version!
Basically, General Relativity is Einstein’s Theory of Gravitation. It is a geometrization of gravity, “GEOMETRODYNAMICS”.
General Relativity: The “Brief” Version!
Basically, General Relativity is Einstein’s Theory of Gravitation. It is a geometrization of gravity, “GEOMETRODYNAMICS”.
The basic idea is that matter induces curvature upon spacetime, and spacetime “tells” that matter how to move.
General Relativity: The “Brief” Version!
Basically, General Relativity is Einstein’s Theory of Gravitation. It is a geometrization of gravity, “GEOMETRODYNAMICS”.
The basic idea is that matter induces curvature upon spacetime, and spacetime “tells” that matter how to move.
In general, we would like to obey the following requirements:
(a)Any field equations describing the theory should be independent of coordinate systems of the laws of nature, and, hence, should be TENSOR equations
(a)Any field equations describing the theory should be independent of coordinate systems of the laws of nature, and, hence, should be TENSOR equations
(b)Similar to other field equations of physics, the field equations should be PDEs of at most second-order for the functions to be determined, which are LINEAR in the highest derivatives.
(a)Any field equations describing the theory should be independent of coordinate systems of the laws of nature, and, hence, should be TENSOR equations
(b)Similar to other field equations of physics, the field equations should be PDEs of at most second-order for the functions to be determined, which are LINEAR in the highest derivatives.
(c)In the appropriate limit, they should reduce the Newton’s law of gravitation
(a)Any field equations describing the theory should be independent of coordinate systems of the laws of nature, and, hence, should be TENSOR equations
(b)Similar to other field equations of physics, the field equations should be PDEs of at most second-order for the functions to be determined, which are LINEAR in the highest derivatives.
(c)In the appropriate limit, they should reduce the Newton’s law of gravitation
(d)The energy-momentum tensor Tab is the S.R. analogue of mass density, and hence, should be the source of the gravitational field.
(a)Any field equations describing the theory should be independent of coordinate systems of the laws of nature, and, hence, should be TENSOR equations
(b)Similar to other field equations of physics, the field equations should be PDEs of at most second-order for the functions to be determined, which are LINEAR in the highest derivatives.
(c)In the appropriate limit, they should reduce the Newton’s law of gravitation
(d)The energy-momentum tensor Tab is the S.R. analogue of mass density, and hence, should be the source of the gravitational field.
(e)Indeed, if the spacetime is flat, Tab should vanish.
Implications:
Implications:a) => Need a tensor that has only derivatives of the metric tensor up to second order.
Implications:a) => Need a tensor that has only derivatives of the metric tensor up to second order.
Implications:a) => Need a tensor that has only derivatives of the metric tensor up to second order.
b) => This tensor, The Einstein tensor Gmn must then be built out of the curvature tensor, metric tensor, and ℇ-tensor.
Implications:a) => Need a tensor that has only derivatives of the metric tensor up to second order.
b) => This tensor, The Einstein tensor Gmn must then be built out of the curvature tensor, metric tensor, and ℇ-tensor.
Implications Continued...
Implications Continued...Conservation of energy requires that:
Implications Continued...Conservation of energy requires that:
Tmn;n = 0 ) Gmn
;n = 0
Implications Continued...Conservation of energy requires that:
Tmn;n = 0 ) Gmn
;n = 0
One can show rigorously that there is only ONE 2nd-rank tensor which is linear
(requirement (b)) in the components of the curvature tensor and which satisfies this
relationship:
Implications Continued...Conservation of energy requires that:
Tmn;n = 0 ) Gmn
;n = 0
One can show rigorously that there is only ONE 2nd-rank tensor which is linear
(requirement (b)) in the components of the curvature tensor and which satisfies this
relationship:
Gmn = Rmn � 1
2gmnR+ ⇤gmn = Tmn
Implications Continued...Conservation of energy requires that:
Tmn;n = 0 ) Gmn
;n = 0
One can show rigorously that there is only ONE 2nd-rank tensor which is linear
(requirement (b)) in the components of the curvature tensor and which satisfies this
relationship:
Gmn = Rmn � 1
2gmnR+ ⇤gmn = Tmn
⋀ - Cosmological Constant (We will set this to zero)
The Einstein Field Equations
The Einstein Field Equations
We thus arrive at The Einstein Field equations:
The Einstein Field Equations
We thus arrive at The Einstein Field equations:
Rmn � 1
2gmnR = Tmn
The Einstein Field Equations
We thus arrive at The Einstein Field equations:
Rmn � 1
2gmnR = Tmn
Derived by Einstein after 10 years of research in 1915.
The Einstein Field Equations
We thus arrive at The Einstein Field equations:
Rmn � 1
2gmnR = Tmn
Derived by Einstein after 10 years of research in 1915.
These constitute a system of ten, nonlinear, coupled, hyperbolic PDEs to determine the ten metric functions. In general, no unique solution
exists.
The Einstein Field Equations
The Einstein Field Equations
Historical Note: In 1915, Hilbert also derived the field equations in a more
rigorous manner, but, Einstein beat him to the punch!
Just for kicks...
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
�SG =1
2
Z
M
p�g
✓Ruv �
1
2Rguv
◆�g
uvd
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
�SG =1
2
Z
M
p�g
✓Ruv �
1
2Rguv
◆�g
uvd
4x
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
�SG =1
2
Z
M
p�g
✓Ruv �
1
2Rguv
◆�g
uvd
4x
�SG = 0 ) Ruv �1
2Rguv = 0
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
�SG =1
2
Z
M
p�g
✓Ruv �
1
2Rguv
◆�g
uvd
4x
�SG = 0 ) Ruv �1
2Rguv = 0
Just for kicks...SG =
1
2
Z
MR
p�gd
4x
SG =1
2
Z
M
�Ruvg
uvp�g
�d
4x
�SG =1
2
Z
M
�g
uvp�g�Ruv +Ruv�⇥g
uvp�g
⇤�d
4x
After Much Computation...
�SG =1
2
Z
M
p�g
✓Ruv �
1
2Rguv
◆�g
uvd
4x
�SG = 0 ) Ruv �1
2Rguv = 0 Vacuum Field
Equations!
Just for kicks...
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:� (SG + Sm) = 0
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:� (SG + Sm) = 0
One can show that:
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:� (SG + Sm) = 0
One can show that:�Sm = 0 = �1
2
Z
MTuv
p�g�g
uvd
4x
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:� (SG + Sm) = 0
One can show that:�Sm = 0 = �1
2
Z
MTuv
p�g�g
uvd
4x
Combining this with our previous derivation, we obtain:
Just for kicks...If you want to include matter, you must consider a variational principle
of the form:� (SG + Sm) = 0
One can show that:�Sm = 0 = �1
2
Z
MTuv
p�g�g
uvd
4x
Combining this with our previous derivation, we obtain:
Ruv �1
2Rguv = Tuv
A Quick Note on Curvature
A Quick Note on Curvature
We have so far heavily relied on the notion of a curvature tensor, but have not really explained why we need it, except for the bit about matter inducing curvature, and so forth...
It has to do with the underlying geometry of General Relativity.
A Quick Note on Curvature
In classical physics, the underlying geometry is Euclidean, which is a flat-space geometry.
That is, when we wish to make measurements in a lab, we place a coordinate system over our experiment, and make computations with respect to elements of the Euclidean vector space.
A Quick Note on Curvature
A Quick Note on Curvature
A Quick Note on Curvature
A Quick Note on Curvature
A Quick Note on Curvature
A Quick Note on Curvature
x
A Quick Note on Curvature
x
y
A Quick Note on Curvature
x
y
z
A Quick Note on Curvature
x
y
z
A Quick Note on Curvature
x
y
z
P1
A Quick Note on Curvature
x
y
z
P1
A Quick Note on Curvature
x
y
z
P1P2
A Quick Note on Curvature
x
y
z
P1P2
In Euclidean space, distance between any two points:
A Quick Note on Curvature
x
y
z
P1P2
In Euclidean space, distance between any two points:ds
2 = (dx1)2 + (dx2)2 + (dx3)2 + ...
A Quick Note on Curvature
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
ds
2 = ⌘abdxadx
b = �dt
2 + dx
2 + dy
2 + dz
2
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
ds
2 = ⌘abdxadx
b = �dt
2 + dx
2 + dy
2 + dz
2
⌘ab = ⌘ab = diag(�1, 1, 1, 1)
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
ds
2 = ⌘abdxadx
b = �dt
2 + dx
2 + dy
2 + dz
2
⌘ab = ⌘ab = diag(�1, 1, 1, 1)
Einstein: In a more general theory, the metric tensor is actually a function of the coordinates, and NOT constant:
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
ds
2 = ⌘abdxadx
b = �dt
2 + dx
2 + dy
2 + dz
2
⌘ab = ⌘ab = diag(�1, 1, 1, 1)
Einstein: In a more general theory, the metric tensor is actually a function of the coordinates, and NOT constant:
ds
2 = gabdxadx
b
A Quick Note on Curvature
Can Generalize this to Minkowsi Space of Special Relativity:
ds
2 = ⌘abdxadx
b = �dt
2 + dx
2 + dy
2 + dz
2
⌘ab = ⌘ab = diag(�1, 1, 1, 1)
Einstein: In a more general theory, the metric tensor is actually a function of the coordinates, and NOT constant:
ds
2 = gabdxadx
b
g
ab = f(x0, x
1, x
2, x
3)
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers:
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping:
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
M N
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
M NThis is a 1:1 mapping:
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
M NThis is a 1:1 mapping: x 6= y ) f(x) 6= f(y)
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
M NThis is a 1:1 mapping: x 6= y ) f(x) 6= f(y)
Which means that f has a well-defined inverse:
General Relativity is then a theory in which the metric tensor is not constant, which implies that a pseudo-Riemannian manifold must be used as the underlying geometry.Rn :Succession of n real numbers: (x1
, . . . , x
n)
We define the mapping: f : M ! N
M NThis is a 1:1 mapping: x 6= y ) f(x) 6= f(y)
Which means that f has a well-defined inverse:
f�1 : N ! M
A manifold M is a space satisfying:
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
The family of open neighbourhoods cover the whole of M :
[
i
Ui = M
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
The family of open neighbourhoods cover the whole of M :
[
i
Ui = M
There exist mappings � : U ! Rn.
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
The family of open neighbourhoods cover the whole of M :
[
i
Ui = M
There exist mappings � : U ! Rn.
Q 2 M ) �(Q) = (x1, . . . , x
n) 2 Rn
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
The family of open neighbourhoods cover the whole of M :
[
i
Ui = M
There exist mappings � : U ! Rn.
Q 2 M ) �(Q) = (x1, . . . , x
n) 2 Rn
This mapping is called a coordinate system, U is the coordinate region in M
A manifold M is a space satisfying:
9 a family of open neighbourhoods Ui together with continuous 1-to-1 mappings
fi : Ui ! Rnwith a continuous inverse for a number n
The family of open neighbourhoods cover the whole of M :
[
i
Ui = M
There exist mappings � : U ! Rn.
Q 2 M ) �(Q) = (x1, . . . , x
n) 2 Rn
This mapping is called a coordinate system, U is the coordinate region in M
Can go forward and define coordinate transformations, tangent space, basis vectors, and so
on, but, won’t have enough time!
Summary of Prerequisites
Summary of Prerequisites
The main point is that all of this geometric structure is the fundamental, underlying structure for General Relativity.
It naturally defines a metric tensor on a pseudo-Riemannian manifold:
pseudo-Riemannian:
Summary of Prerequisites
The main point is that all of this geometric structure is the fundamental, underlying structure for General Relativity.
It naturally defines a metric tensor on a pseudo-Riemannian manifold:
pseudo-Riemannian:pg = ±1
⇠a;b + ⇠b;a = 0
Summary of Prerequisites
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant Derivative
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTn
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTn
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTn
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensors
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
Ricci
⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
RicciRmq = Rs
msq = �Rsmqs ; Rm
m = R⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
RicciRmq = Rs
msq = �Rsmqs ; Rm
m = R⇠a;b + ⇠b;a = 0
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
RicciRmq = Rs
msq = �Rsmqs ; Rm
m = R⇠a;b + ⇠b;a = 0
Killing’s Equation
Summary of PrerequisitesThe metric tensor leads to the definition of
fundamental quantities:
Christoffel Symbols�amn =
1
2gab (gbm,n + gbn,m � gmn,b)
Geodesic Equationx
a + �abcx
bx
c = 0
Covariant DerivativeTa;m = Ta,m � �n
amTnCurvature Tensorsam;s;q � am;q;s = abR
bmsq
Riemann
Rbmsq = �b
mq,s � �bms,q + �b
ns�nmq � �b
nq�nms
RicciRmq = Rs
msq = �Rsmqs ; Rm
m = R⇠a;b + ⇠b;a = 0
Killing’s Equation
Developing a Cosmological Model
Developing a Cosmological Model
The present-day universe is modeled with great accuracy by The Friedmann-LeMaitre-
Robertson-Walker (FLRW) metric:
Developing a Cosmological Model
The present-day universe is modeled with great accuracy by The Friedmann-LeMaitre-
Robertson-Walker (FLRW) metric:
ds2 = �dt2 + a2(t)
dr2
1� kr2+ r2
�d✓2 + sin2 ✓d�2
��
Developing a Cosmological Model
The present-day universe is modeled with great accuracy by The Friedmann-LeMaitre-
Robertson-Walker (FLRW) metric:
ds2 = �dt2 + a2(t)
dr2
1� kr2+ r2
�d✓2 + sin2 ✓d�2
��
Developing a Cosmological Model
The present-day universe is modeled with great accuracy by The Friedmann-LeMaitre-
Robertson-Walker (FLRW) metric:
ds2 = �dt2 + a2(t)
dr2
1� kr2+ r2
�d✓2 + sin2 ✓d�2
��
Cosmological scale factor - Describes expansion/collapse behaviour of the
universe.
Developing a Cosmological Model
The present-day universe is modeled with great accuracy by The Friedmann-LeMaitre-
Robertson-Walker (FLRW) metric:
ds2 = �dt2 + a2(t)
dr2
1� kr2+ r2
�d✓2 + sin2 ✓d�2
��
Cosmological scale factor - Describes expansion/collapse behaviour of the
universe.
These models are spatially homogeneous
and isotropic
Cosmological Principle: The large-scale universe can be foliated into a family of space-like hypersurfaces, in which, physical quantities remain constant on each hypersurface, and are only functions of time.
Cosmological Principle: The large-scale universe can be foliated into a family of space-like hypersurfaces, in which, physical quantities remain constant on each hypersurface, and are only functions of time. ta
Cosmological Principle: The large-scale universe can be foliated into a family of space-like hypersurfaces, in which, physical quantities remain constant on each hypersurface, and are only functions of time. ta
⌃1
⌃2
⌃3
⌃n
R4
R⇥ ⌃t
Early-Universe Cosmology
Early-Universe CosmologyEven though the universe is observed to be 99.999 (1-10-5)% isotropic today, minor anisotropies indicate that after the Big Bang, the universe was in a chaotic state, and, in general, was anisotropic.
Early-Universe CosmologyEven though the universe is observed to be 99.999 (1-10-5)% isotropic today, minor anisotropies indicate that after the Big Bang, the universe was in a chaotic state, and, in general, was anisotropic.
Somehow, these anisotropies smoothed out to the present-day universe.
Early-Universe CosmologyEven though the universe is observed to be 99.999 (1-10-5)% isotropic today, minor anisotropies indicate that after the Big Bang, the universe was in a chaotic state, and, in general, was anisotropic.
Somehow, these anisotropies smoothed out to the present-day universe.
Early-universe cosmology, assumes that the universe, although, spatially homogeneous, was anisotropic.
Foundations of Spatial Homogeneity
Foundations of Spatial Homogeneity
Basically, a space is homogeneous if it admits a group of motions. That is, a space is topologically homogeneous if you can carry one point to any
other point via an isometry.
Foundations of Spatial Homogeneity
Basically, a space is homogeneous if it admits a group of motions. That is, a space is topologically homogeneous if you can carry one point to any
other point via an isometry.Isom(M) ⌘ {� : M ! M |� isometry}
Foundations of Spatial Homogeneity
Basically, a space is homogeneous if it admits a group of motions. That is, a space is topologically homogeneous if you can carry one point to any
other point via an isometry.Isom(M) ⌘ {� : M ! M |� isometry}
We can therefore say that a space is homogeneous if for each pair of points
Foundations of Spatial Homogeneity
Basically, a space is homogeneous if it admits a group of motions. That is, a space is topologically homogeneous if you can carry one point to any
other point via an isometry.Isom(M) ⌘ {� : M ! M |� isometry}
We can therefore say that a space is homogeneous if for each pair of points
(p, q) 2 M, 9� 2 Isom(M) such that �(p) = q
Foundations of Spatial Homogeneity
Foundations of Spatial Homogeneity
We will proceed by choosing a basis:
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
L⇠j [ei, ek] = 0
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
L⇠j [ei, ek] = 0
This basis then spans a Lie Algebra
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
L⇠j [ei, ek] = 0
This basis then spans a Lie Algebra
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
L⇠j [ei, ek] = 0
This basis then spans a Lie AlgebraTo construct a homogeneous space, we define
a left-invariant frame:
Foundations of Spatial Homogeneity
We will proceed by choosing a basis: ei at p 2 M
L⇠j [ei, ek] = 0
This basis then spans a Lie AlgebraTo construct a homogeneous space, we define
a left-invariant frame:
[ei, ej ] = Ckijek
[ei, ej ] = Ckijek
[ei, ej ] = Ckijek
[ei, ej ] = Ckijek
Structure Constants of The Group
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define:
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k Dual basis to:
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k Dual basis to:ek
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k Dual basis to:ek
ds2 = gij!i ⌦ !j
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k Dual basis to:ek
ds2 = gij!i ⌦ !j
[ei, ej ] = Ckijek
Structure Constants of The Group
Now, define: !k Dual basis to:ek
ds2 = gij!i ⌦ !j
This is the metric tensor of a homogeneous space.
The Bianchi Classifications
The Bianchi Classifications
There are 9 such classifications of homogeneous spacetimes (with an isometry group of dimension 3), these are The Bianchi Classifications, named after Luigi Bianchi (1898).
The Bianchi Classifications
There are 9 such classifications of homogeneous spacetimes (with an isometry group of dimension 3), these are The Bianchi Classifications, named after Luigi Bianchi (1898).
Essentially, one solves for the Killing vectors/differential one-forms, which then give the form of the metric tensor.
Table 8.2. Killing vectors and reciprocal group generators by Bianchi type
Expressions are given in canonical coordinates: for full explanation, see text.
I II IV V VI (including III ) VIIξA ∂x ∂x ∂x − y∂y − (y + z)∂z ∂x − y∂y − z∂z ∂x + (z −Ay)∂y ∂x + (z −Ay)∂y
+ (y −Az)∂z − (y + Az)∂z∂y ∂y ∂y ∂y ∂y ∂y∂z ∂z + y∂x ∂z ∂z ∂z ∂z
ηA ∂x ∂x ∂x ∂x ∂x ∂x∂y ∂y + z∂x e−x(∂y − x∂z) e−x∂y e−Ax(coshx ∂y + sinhx ∂z) e−Ax(cosx ∂y − sinx ∂z)∂z ∂z e−x∂z e−x∂z e−Ax(sinhx ∂y + coshx ∂z) e−Ax(sinx ∂y + cosx ∂z)
ωA dx dx− z dy dx dx dx dxdy dy exdy exdy eAx(coshxdy − sinhxdz) eAx(cosxdy − sinxdz)dz dz ex(dz + xdy) exdz eAx(− sinhxdy + coshxdz) eAx(sinxdy + cosxdz)
VIII IXξA sech y cosh z ∂x + sinh z ∂y − tanh y cosh z ∂z sec y cos z ∂x + sin z ∂y − tan y cos z ∂z
sech y sinh z ∂x + cosh z ∂y − tanh y sinh z ∂z − sec y sin z ∂x + cos z ∂y + tan y sin z ∂z∂z ∂z
ηA ∂x ∂x− sinx tanh y ∂x + cosx ∂y − sinx sech y ∂z sinx tan y ∂x + cosx ∂y − sinx sec y ∂zcosx tanh y ∂x + sinx ∂y + cosx sech y ∂z − cosx tan y ∂x + sinx ∂y + cosx sec y ∂z
ωA dx− sinh y dz dx + sin y dzcosxdy − sinx cosh y dz cosxdy − sinx cos y dzsinxdy + cosx cosh y dz sinxdy + cosx cos y dz
Table 8.2. Killing vectors and reciprocal group generators by Bianchi type
Expressions are given in canonical coordinates: for full explanation, see text.
I II IV V VI (including III ) VIIξA ∂x ∂x ∂x − y∂y − (y + z)∂z ∂x − y∂y − z∂z ∂x + (z −Ay)∂y ∂x + (z −Ay)∂y
+ (y −Az)∂z − (y + Az)∂z∂y ∂y ∂y ∂y ∂y ∂y∂z ∂z + y∂x ∂z ∂z ∂z ∂z
ηA ∂x ∂x ∂x ∂x ∂x ∂x∂y ∂y + z∂x e−x(∂y − x∂z) e−x∂y e−Ax(coshx ∂y + sinhx ∂z) e−Ax(cosx ∂y − sinx ∂z)∂z ∂z e−x∂z e−x∂z e−Ax(sinhx ∂y + coshx ∂z) e−Ax(sinx ∂y + cosx ∂z)
ωA dx dx− z dy dx dx dx dxdy dy exdy exdy eAx(coshxdy − sinhxdz) eAx(cosxdy − sinxdz)dz dz ex(dz + xdy) exdz eAx(− sinhxdy + coshxdz) eAx(sinxdy + cosxdz)
VIII IXξA sech y cosh z ∂x + sinh z ∂y − tanh y cosh z ∂z sec y cos z ∂x + sin z ∂y − tan y cos z ∂z
sech y sinh z ∂x + cosh z ∂y − tanh y sinh z ∂z − sec y sin z ∂x + cos z ∂y + tan y sin z ∂z∂z ∂z
ηA ∂x ∂x− sinx tanh y ∂x + cosx ∂y − sinx sech y ∂z sinx tan y ∂x + cosx ∂y − sinx sec y ∂zcosx tanh y ∂x + sinx ∂y + cosx sech y ∂z − cosx tan y ∂x + sinx ∂y + cosx sec y ∂z
ωA dx− sinh y dz dx + sin y dzcosxdy − sinx cosh y dz cosxdy − sinx cos y dzsinxdy + cosx cosh y dz sinxdy + cosx cos y dz
From Stephani’s Text - Exact Solutions of Einstein’s Field Equations, 2003
Table 8.2. Killing vectors and reciprocal group generators by Bianchi type
Expressions are given in canonical coordinates: for full explanation, see text.
I II IV V VI (including III ) VIIξA ∂x ∂x ∂x − y∂y − (y + z)∂z ∂x − y∂y − z∂z ∂x + (z −Ay)∂y ∂x + (z −Ay)∂y
+ (y −Az)∂z − (y + Az)∂z∂y ∂y ∂y ∂y ∂y ∂y∂z ∂z + y∂x ∂z ∂z ∂z ∂z
ηA ∂x ∂x ∂x ∂x ∂x ∂x∂y ∂y + z∂x e−x(∂y − x∂z) e−x∂y e−Ax(coshx ∂y + sinhx ∂z) e−Ax(cosx ∂y − sinx ∂z)∂z ∂z e−x∂z e−x∂z e−Ax(sinhx ∂y + coshx ∂z) e−Ax(sinx ∂y + cosx ∂z)
ωA dx dx− z dy dx dx dx dxdy dy exdy exdy eAx(coshxdy − sinhxdz) eAx(cosxdy − sinxdz)dz dz ex(dz + xdy) exdz eAx(− sinhxdy + coshxdz) eAx(sinxdy + cosxdz)
VIII IXξA sech y cosh z ∂x + sinh z ∂y − tanh y cosh z ∂z sec y cos z ∂x + sin z ∂y − tan y cos z ∂z
sech y sinh z ∂x + cosh z ∂y − tanh y sinh z ∂z − sec y sin z ∂x + cos z ∂y + tan y sin z ∂z∂z ∂z
ηA ∂x ∂x− sinx tanh y ∂x + cosx ∂y − sinx sech y ∂z sinx tan y ∂x + cosx ∂y − sinx sec y ∂zcosx tanh y ∂x + sinx ∂y + cosx sech y ∂z − cosx tan y ∂x + sinx ∂y + cosx sec y ∂z
ωA dx− sinh y dz dx + sin y dzcosxdy − sinx cosh y dz cosxdy − sinx cos y dzsinxdy + cosx cosh y dz sinxdy + cosx cos y dz
From Stephani’s Text - Exact Solutions of Einstein’s Field Equations, 2003
Bianchi Type IV
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
ds
2 = �dt
2 + �ij(t)dxidx
j
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
ds
2 = �dt
2 + �ij(t)dxidx
j
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
dx
1= dx, dx
2= expxdy, dx
3= expx (dz + xdy)
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
dx
1= dx, dx
2= expxdy, dx
3= expx (dz + xdy)
ds
2= �dt
2+ a
2(t)dx
2+ dy
2�b
2(t) exp(2x) + c
2(t) exp(2x)x
2�+ dz
2c
2(t) exp(2x)+
2c
2(t) exp(2x)xdzdy
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
dx
1= dx, dx
2= expxdy, dx
3= expx (dz + xdy)
ds
2= �dt
2+ a
2(t)dx
2+ dy
2�b
2(t) exp(2x) + c
2(t) exp(2x)x
2�+ dz
2c
2(t) exp(2x)+
2c
2(t) exp(2x)xdzdy
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
dx
1= dx, dx
2= expxdy, dx
3= expx (dz + xdy)
ds
2= �dt
2+ a
2(t)dx
2+ dy
2�b
2(t) exp(2x) + c
2(t) exp(2x)x
2�+ dz
2c
2(t) exp(2x)+
2c
2(t) exp(2x)xdzdy
For:
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Bianchi Type IVWe are interested in a Bianchi Type IV (BIV) model, so we take the “naive” approach of forming the metric tensor from the differential forms from the previous page:
dx
1= dx, dx
2= expxdy, dx
3= expx (dz + xdy)
ds
2= �dt
2+ a
2(t)dx
2+ dy
2�b
2(t) exp(2x) + c
2(t) exp(2x)x
2�+ dz
2c
2(t) exp(2x)+
2c
2(t) exp(2x)xdzdy
For:
�ab(t) = diag�a2(t), b2(t), c2(t)
�
ds
2 = �dt
2 + �ij(t)dxidx
j
Time-dependent scaling function
Computing The Einstein Field Equations in this coordinate basis gives very complicated results!
Computing The Einstein Field Equations in this coordinate basis gives very complicated results!
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors:
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea cauv = �avu � �a
uv
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea cauv = �avu � �a
uv
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea cauv = �avu � �a
uv �auv =1
2
�gabc
bvu + guvc
bav � gvbc
bau
�
These expressions are too complicated for our liking... But, G.R. is a COVARIANT
theory, it shouldn’t matter what coordinate system we use, we will therefore take the approach of
ORTHONORMAL FRAMES.
That is, we choose a basis such that all four basis vectors: {eu}
are mutually orthonormal. Thus,g(eu, ev) = ⌘uv = �uv = diag(�1, 1, 1, 1)
The structure constants from before, are now functions, and satisfy:
[eu, ev] = cauvea cauv = �avu � �a
uv �auv =1
2
�gabc
bvu + guvc
bav � gvbc
bau
�
These are all now independent of coordinate functions!
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
Where:
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
hab ⌘ gab � uaub
ucucWhere:
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
hab ⌘ gab � uaub
ucucWhere: is the projection
tensor.
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
hab ⌘ gab � uaub
ucucWhere: is the projection
tensor.Define: ↵ = �ucuc
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
hab ⌘ gab � uaub
ucucWhere: is the projection
tensor.Define: ↵ = �ucuc
T ab = (µ+ p)uaub � ucucgabp
Before we continue, it is necessary to discuss the matter source of interest, particularly, we need to develop the theory behind a viscous fluid tensor.
Start with a pressure-less fluid:T00 = µu0u0 ) Tab = µuaub
Assuming there is a pressure (which only acts on the spatial components):
Tab = µuaub + ↵phab (↵ = ±1)
hab ⌘ gab � uaub
ucucWhere: is the projection
tensor.Define: ↵ = �ucuc
T ab = (µ+ p)uaub � ucucgabp
This is the energy-momentum tensor for a perfect fluid.
Let the viscous contributions be denoted as:
Let the viscous contributions be denoted as: Vab
Let the viscous contributions be denoted as: Vab
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ik
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ik
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ik
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ikStress tensor
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ikStress tensor
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ikStress tensor
Let the viscous contributions be denoted as: Vab
Tab = wuaub � ucucgabp+ Vab
From classical fluid mechanics, the Euler equation is:(⇢ui),t = �⇧ik,k
Where:⇧ik = p�ik + ⇢uiuk
is the momentum flux tensor.We will add on a term that represents the viscous
momentum flux:⇧ik = p�ik + ⇢uiuk � ⌃0
ik = �⌃ik + ⇢uiuk
Where:⌃ik = �p�ik + ⌃0
ikStress tensor
Viscous stress tensor
One can show that the most general viscous tensor can be formed as:
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
Shear viscosity
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
Shear viscosity
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
Shear viscosity Bulk viscosity
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
Shear viscosity Bulk viscosity
Note that:
One can show that the most general viscous tensor can be formed as:
⌃0ik = ⌘
✓ui,k + uk,i �
2
3�ikul,l
◆+ ⇠�ikul,l
Shear viscosity Bulk viscosity
Note that:
�ikul,l ⌘ ✓
✓ui,k + uk,i �
2
3�ikul,l
◆⌘ �ab
Expansion Rate Tensor
Shear Rate Tensor
We then have:
We then have:Vab = �2⌘�ab � ⇠✓hab
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:T ab;b = 0 = T b
a;b
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:T ab;b = 0 = T b
a;b
We derive an equation of motion for the fluid:
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:T ab;b = 0 = T b
a;b
We derive an equation of motion for the fluid:
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:T ab;b = 0 = T b
a;b
We derive an equation of motion for the fluid:
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
Where we have defined:
We then have:Vab = �2⌘�ab � ⇠✓hab
And Finally:Tab = (µ+ p)uaub � ucu
cgabp� 2⌘�ab � ⇠✓hab
Using the energy conservation law:T ab;b = 0 = T b
a;b
We derive an equation of motion for the fluid:
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
Where we have defined: ⇡ab = 2⌘�ab
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0✓�2 =
1
2�ab�ab ) �ab�ab = 2�2
◆
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0✓�2 =
1
2�ab�ab ) �ab�ab = 2�2
◆
We assume that cosmological fluids obey the barotropic equation of state:
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0✓�2 =
1
2�ab�ab ) �ab�ab = 2�2
◆
We assume that cosmological fluids obey the barotropic equation of state:
p = wµ,w 2 R
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0✓�2 =
1
2�ab�ab ) �ab�ab = 2�2
◆
We assume that cosmological fluids obey the barotropic equation of state:
p = wµ,w 2 RFor relativistic particles in the early universe, w = 1/3, (See: Landau and Lifshitz, “Fluid Mechanics” or Ellis,
Maartens, MacCallum “Relativistic Cosmology”)
ua�(µ+ p)uau
b + �bap� ⇡ba � ⇠✓
��ba + uau
b��
;b= 0
We evaluate this expression term-by-term, and obtain:
µ+ (µ+ p)✓ � 4⌘�2 � ⇠✓2 = 0✓�2 =
1
2�ab�ab ) �ab�ab = 2�2
◆
We assume that cosmological fluids obey the barotropic equation of state:
p = wµ,w 2 RFor relativistic particles in the early universe, w = 1/3, (See: Landau and Lifshitz, “Fluid Mechanics” or Ellis,
Maartens, MacCallum “Relativistic Cosmology”)
µ+
✓4
3µ
◆✓ � 4⌘�2 � ⇠✓2 = 0
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
The Strong Energy Condition (SEC) is:
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
The Strong Energy Condition (SEC) is:✓T ab � 1
2Tgab
◆uaub � 0
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
The Strong Energy Condition (SEC) is:✓T ab � 1
2Tgab
◆uaub � 0
By The Einstein Field Equations, we have:
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
The Strong Energy Condition (SEC) is:✓T ab � 1
2Tgab
◆uaub � 0
By The Einstein Field Equations, we have:Rabuaub � 0
We will also assume energy conditions for our fluid, which will allow us to build the arguments for the
existence/non-existence of a past singularity for this cosmological model (at the end).
The Weak Energy Condition (WEC) is:T abuaub � 0
This basically says that any observer will always observe a positive energy density.
The Strong Energy Condition (SEC) is:✓T ab � 1
2Tgab
◆uaub � 0
By The Einstein Field Equations, we have:Rabuaub � 0
More on these things later.
Back To The Einstein Field Equations!
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:
Back To The Einstein Field Equations!
The properties of a fluid flow in a spacetime can be described by the decomposition:ua;b = �aaub + �ab + !ab +
1
3hab✓
Congruence of fluid lines moving with 4-velocity:ua
ua;b = �aaub + �ab + !ab +1
3hab✓
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
Shear Tensor: Measures how much the fluid congruence deforms.
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
Shear Tensor: Measures how much the fluid congruence deforms.
!ab =1
2(um;n � un;m)hm
a hnb
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
Shear Tensor: Measures how much the fluid congruence deforms.
!ab =1
2(um;n � un;m)hm
a hnb
ua;b = �aaub + �ab + !ab +1
3hab✓
✓ ⌘ ua;a
Expansion Tensor: Measures divergence of the fluid congruence.
aa ⌘ ua;bub Fluid Acceleration: Measures how
much the fluid congruence can be taken to be non-geodesic.
�ab =
1
2(um;n + un;m)� 1
3uc;chmn
�hma hn
b
Shear Tensor: Measures how much the fluid congruence deforms.
!ab =1
2(um;n � un;m)hm
a hnb
Vorticity Tensor: Measures how much the fluid congruence rotates.
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
ckij = ✏ijlnlk + al
��li�
kj � �lj�
ki
�
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
ckij = ✏ijlnlk + al
��li�
kj � �lj�
ki
�
The structure constants from before (now functions) are purely spatial, and are constant on each spatial
slice.
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
ckij = ✏ijlnlk + al
��li�
kj � �lj�
ki
�
The structure constants from before (now functions) are purely spatial, and are constant on each spatial
slice.
So:
Connecting this to our orthonormal frame approach, we assume that
the fluid is non-tilted:!uv = uu;vu
v = 0
✓uv = uu;v =1
3✓huv + �uv
ckij = ✏ijlnlk + al
��li�
kj � �lj�
ki
�
The structure constants from before (now functions) are purely spatial, and are constant on each spatial
slice.
So:nlk, ai are purely functions of time.
Applying The Jacobi identity as applied to the set of vectors:
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
@t(ckab) + cktdc
dab + ckadc
dbt + ckbdc
dta = 0
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
@t(ckab) + cktdc
dab + ckadc
dbt + ckbdc
dta = 0
One can show that upon applying The Jacobi identity to the three
spatial vectors, we obtain:
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
@t(ckab) + cktdc
dab + ckadc
dbt + ckbdc
dta = 0
One can show that upon applying The Jacobi identity to the three
spatial vectors, we obtain:nijai = 0
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
@t(ckab) + cktdc
dab + ckadc
dbt + ckbdc
dta = 0
One can show that upon applying The Jacobi identity to the three
spatial vectors, we obtain:nijai = 0
Applying The Jacobi identity as applied to the set of vectors:
(U = @t, ea, eb)
We get:[U, [ea, eb]] + [ea, [eb,U]] + [eb, [U, ea]] = 0
@t(ckab) + cktdc
dab + ckadc
dbt + ckbdc
dta = 0
One can show that upon applying The Jacobi identity to the three
spatial vectors, we obtain:nijai = 0
Condition for Lie Algebra property to hold.
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:catb = �✓ab + ✏abc⌦
c
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:catb = �✓ab + ✏abc⌦
c
⌦a =1
2✏abcdubec · ed
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:catb = �✓ab + ✏abc⌦
c
⌦a =1
2✏abcdubec · ed
In combination with the previous definitions in the Jacobi identity, we get:
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:catb = �✓ab + ✏abc⌦
c
⌦a =1
2✏abcdubec · ed
In combination with the previous definitions in the Jacobi identity, we get:
ai +1
3✓ai + �ija
j + ✏ijkaj⌦k = 0
It is important to note that we always take to be a symmetric matrix and as such we can diagonalize it using a orientation of our choice for the spatial frame. It has been
conventional to assume:
nij
nij = diag(n1, n2, n3), , ai = (0, 0, a)
Further, using the definitions:catb = �✓ab + ✏abc⌦
c
⌦a =1
2✏abcdubec · ed
In combination with the previous definitions in the Jacobi identity, we get:
ai +1
3✓ai + �ija
j + ✏ijkaj⌦k = 0
˙nab +1
3✓nab + 2nk
(a✏b)kl⌦l � 2nk(a�b)
k = 0
One classifies the different Bianchi types by the signs of the eigenvalues:
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and a
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and a15.4 The orthonormal frame approach to the Bianchi models 411
Class Type a n1 n2 n3
A I 0 0 0 0II 0 + 0 0
VI0 0 + − 0VII0 0 + + 0VIII 0 + + −IX 0 + + +
B V + 0 0 0IV + + 0 0
VIh + + − 0VIIh + + + 0
Table 15.2: The Bianchi types in terms of the algebraic properties of the structurecoefficients.
For the structure coefficients eq. (15.62) to correspond to a Lie algebra, thevector ai must according to eq. (15.65) be in the kernel4 of the matrix nij . Forthe class A model, ai = 0 and this equation is identically satisfied. For the classB models, ai must be an eigenvector of the matrix nij with zero eigenvalue. Inany case, since nij is a symmetric matrix, we can diagonalise it using a specificorientation of the spatial frame. Thus, without any loss of generality we canassume that
nij = diag(n1, n2, n3), ai = (0, 0, a) (15.68)
by a suitable choice of frame. The Jacobi identity then implies n3a = 0.The eigenvalues of a matrix are invariant properties of a matrix under con-
jugation with respect to rotations. The Bianchi models can now be charac-terised by the relative signs of the eigenvalues n1, n2, n3 and a. In Table 15.2the classification of the Bianchi types in terms of these eigenvalues is listed.For the types VIh and VIIh the group parameter is defined by the equation
hn1n2 = a2. (15.69)
In this table III=VI−1.Note that for some of the Bianchi types, two or three eigenvalues are equal
to zero. Hence, for these we have unused degrees of freedom to choose theorientation of the spatial frame. For example, the type I case has vanishingstructure coefficients. Thus we have an unused SO(3) rotation for the spatialframe. Since the shear is symmetric, we can choose to diagonalise σab instead.So for a Bianchi type I universe model we can without any loss of generality choosethe shear to be diagonal.
Einstein’s Field Equations for Bianchi type universes
We can use the results from the previous chapter to find the field equationsfor the Bianchi type universe models. The Ricci tensor can be found fromcontracting the Riemann tensor eq. (7.45). Using the four-dimensional Riccitensor we can show that the tt-equation yields Raychaudhuri’s equation, eq.(14.31), and the spatial ab-equations yield the shear propagation equations, eq.(14.40), and the generalised Friedmann equation, eq (14.34). The off-diagonal
4Consider a matrix M and a vector v. The vector v is in the kernel of M if and only if Mv = 0.
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and a15.4 The orthonormal frame approach to the Bianchi models 411
Class Type a n1 n2 n3
A I 0 0 0 0II 0 + 0 0
VI0 0 + − 0VII0 0 + + 0VIII 0 + + −IX 0 + + +
B V + 0 0 0IV + + 0 0
VIh + + − 0VIIh + + + 0
Table 15.2: The Bianchi types in terms of the algebraic properties of the structurecoefficients.
For the structure coefficients eq. (15.62) to correspond to a Lie algebra, thevector ai must according to eq. (15.65) be in the kernel4 of the matrix nij . Forthe class A model, ai = 0 and this equation is identically satisfied. For the classB models, ai must be an eigenvector of the matrix nij with zero eigenvalue. Inany case, since nij is a symmetric matrix, we can diagonalise it using a specificorientation of the spatial frame. Thus, without any loss of generality we canassume that
nij = diag(n1, n2, n3), ai = (0, 0, a) (15.68)
by a suitable choice of frame. The Jacobi identity then implies n3a = 0.The eigenvalues of a matrix are invariant properties of a matrix under con-
jugation with respect to rotations. The Bianchi models can now be charac-terised by the relative signs of the eigenvalues n1, n2, n3 and a. In Table 15.2the classification of the Bianchi types in terms of these eigenvalues is listed.For the types VIh and VIIh the group parameter is defined by the equation
hn1n2 = a2. (15.69)
In this table III=VI−1.Note that for some of the Bianchi types, two or three eigenvalues are equal
to zero. Hence, for these we have unused degrees of freedom to choose theorientation of the spatial frame. For example, the type I case has vanishingstructure coefficients. Thus we have an unused SO(3) rotation for the spatialframe. Since the shear is symmetric, we can choose to diagonalise σab instead.So for a Bianchi type I universe model we can without any loss of generality choosethe shear to be diagonal.
Einstein’s Field Equations for Bianchi type universes
We can use the results from the previous chapter to find the field equationsfor the Bianchi type universe models. The Ricci tensor can be found fromcontracting the Riemann tensor eq. (7.45). Using the four-dimensional Riccitensor we can show that the tt-equation yields Raychaudhuri’s equation, eq.(14.31), and the spatial ab-equations yield the shear propagation equations, eq.(14.40), and the generalised Friedmann equation, eq (14.34). The off-diagonal
4Consider a matrix M and a vector v. The vector v is in the kernel of M if and only if Mv = 0.
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and a15.4 The orthonormal frame approach to the Bianchi models 411
Class Type a n1 n2 n3
A I 0 0 0 0II 0 + 0 0
VI0 0 + − 0VII0 0 + + 0VIII 0 + + −IX 0 + + +
B V + 0 0 0IV + + 0 0
VIh + + − 0VIIh + + + 0
Table 15.2: The Bianchi types in terms of the algebraic properties of the structurecoefficients.
For the structure coefficients eq. (15.62) to correspond to a Lie algebra, thevector ai must according to eq. (15.65) be in the kernel4 of the matrix nij . Forthe class A model, ai = 0 and this equation is identically satisfied. For the classB models, ai must be an eigenvector of the matrix nij with zero eigenvalue. Inany case, since nij is a symmetric matrix, we can diagonalise it using a specificorientation of the spatial frame. Thus, without any loss of generality we canassume that
nij = diag(n1, n2, n3), ai = (0, 0, a) (15.68)
by a suitable choice of frame. The Jacobi identity then implies n3a = 0.The eigenvalues of a matrix are invariant properties of a matrix under con-
jugation with respect to rotations. The Bianchi models can now be charac-terised by the relative signs of the eigenvalues n1, n2, n3 and a. In Table 15.2the classification of the Bianchi types in terms of these eigenvalues is listed.For the types VIh and VIIh the group parameter is defined by the equation
hn1n2 = a2. (15.69)
In this table III=VI−1.Note that for some of the Bianchi types, two or three eigenvalues are equal
to zero. Hence, for these we have unused degrees of freedom to choose theorientation of the spatial frame. For example, the type I case has vanishingstructure coefficients. Thus we have an unused SO(3) rotation for the spatialframe. Since the shear is symmetric, we can choose to diagonalise σab instead.So for a Bianchi type I universe model we can without any loss of generality choosethe shear to be diagonal.
Einstein’s Field Equations for Bianchi type universes
We can use the results from the previous chapter to find the field equationsfor the Bianchi type universe models. The Ricci tensor can be found fromcontracting the Riemann tensor eq. (7.45). Using the four-dimensional Riccitensor we can show that the tt-equation yields Raychaudhuri’s equation, eq.(14.31), and the spatial ab-equations yield the shear propagation equations, eq.(14.40), and the generalised Friedmann equation, eq (14.34). The off-diagonal
4Consider a matrix M and a vector v. The vector v is in the kernel of M if and only if Mv = 0.
We are interested in Bianchi IV:
One classifies the different Bianchi types by the signs of the eigenvalues:
n11, n22, n33 = n1, n2, n3 and a15.4 The orthonormal frame approach to the Bianchi models 411
Class Type a n1 n2 n3
A I 0 0 0 0II 0 + 0 0
VI0 0 + − 0VII0 0 + + 0VIII 0 + + −IX 0 + + +
B V + 0 0 0IV + + 0 0
VIh + + − 0VIIh + + + 0
Table 15.2: The Bianchi types in terms of the algebraic properties of the structurecoefficients.
For the structure coefficients eq. (15.62) to correspond to a Lie algebra, thevector ai must according to eq. (15.65) be in the kernel4 of the matrix nij . Forthe class A model, ai = 0 and this equation is identically satisfied. For the classB models, ai must be an eigenvector of the matrix nij with zero eigenvalue. Inany case, since nij is a symmetric matrix, we can diagonalise it using a specificorientation of the spatial frame. Thus, without any loss of generality we canassume that
nij = diag(n1, n2, n3), ai = (0, 0, a) (15.68)
by a suitable choice of frame. The Jacobi identity then implies n3a = 0.The eigenvalues of a matrix are invariant properties of a matrix under con-
jugation with respect to rotations. The Bianchi models can now be charac-terised by the relative signs of the eigenvalues n1, n2, n3 and a. In Table 15.2the classification of the Bianchi types in terms of these eigenvalues is listed.For the types VIh and VIIh the group parameter is defined by the equation
hn1n2 = a2. (15.69)
In this table III=VI−1.Note that for some of the Bianchi types, two or three eigenvalues are equal
to zero. Hence, for these we have unused degrees of freedom to choose theorientation of the spatial frame. For example, the type I case has vanishingstructure coefficients. Thus we have an unused SO(3) rotation for the spatialframe. Since the shear is symmetric, we can choose to diagonalise σab instead.So for a Bianchi type I universe model we can without any loss of generality choosethe shear to be diagonal.
Einstein’s Field Equations for Bianchi type universes
We can use the results from the previous chapter to find the field equationsfor the Bianchi type universe models. The Ricci tensor can be found fromcontracting the Riemann tensor eq. (7.45). Using the four-dimensional Riccitensor we can show that the tt-equation yields Raychaudhuri’s equation, eq.(14.31), and the spatial ab-equations yield the shear propagation equations, eq.(14.40), and the generalised Friedmann equation, eq (14.34). The off-diagonal
4Consider a matrix M and a vector v. The vector v is in the kernel of M if and only if Mv = 0.
We are interested in Bianchi IV:
ai = a�i3 > 0, and n1 > 0, n2 = n3 = 0
So far, we have reduced The Einstein Field equations into a set of first-order dynamical
equations:
So far, we have reduced The Einstein Field equations into a set of first-order dynamical
equations:µ+
✓4
3µ
◆✓ � 4⌘�2 � ⇠✓2 = 0
So far, we have reduced The Einstein Field equations into a set of first-order dynamical
equations:µ+
✓4
3µ
◆✓ � 4⌘�2 � ⇠✓2 = 0
ai +1
3✓ai + �ija
j + ✏ijkaj⌦k = 0
So far, we have reduced The Einstein Field equations into a set of first-order dynamical
equations:µ+
✓4
3µ
◆✓ � 4⌘�2 � ⇠✓2 = 0
ai +1
3✓ai + �ija
j + ✏ijkaj⌦k = 0
˙nab +1
3✓nab + 2nk
(a✏b)kl⌦l � 2nk(a�b)
k = 0
So far, we have reduced The Einstein Field equations into a set of first-order dynamical
equations:µ+
✓4
3µ
◆✓ � 4⌘�2 � ⇠✓2 = 0
ai +1
3✓ai + �ija
j + ✏ijkaj⌦k = 0
˙nab +1
3✓nab + 2nk
(a✏b)kl⌦l � 2nk(a�b)
k = 0
We are not done! The system above has unspecified functions for the expansion scalar, and the shear tensor. To close the system, we need dynamical
equations for these as well.
The Raychaudhuri Equation for Viscous Flow
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:ua;d;b � ua
;b;d = �Racdbu
c
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:ua;d;b � ua
;b;d = �Racdbu
c
Can show that:
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:ua;d;b � ua
;b;d = �Racdbu
c
Can show that:d✓
dt= �Rbcu
buc + aa;a + 2!2 � 2�2 � 1
3✓2
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:ua;d;b � ua
;b;d = �Racdbu
c
Can show that:d✓
dt= �Rbcu
buc + aa;a + 2!2 � 2�2 � 1
3✓2
Since:
The Raychaudhuri Equation for Viscous Flow
We are interested in analyzing the equation:d✓
dt=
�ua;a
�;bub = ua
;a;bub
By the definition of The Riemann curvature tensor:ua;d;b � ua
;b;d = �Racdbu
c
Can show that:d✓
dt= �Rbcu
buc + aa;a + 2!2 � 2�2 � 1
3✓2
Since:
Rab =
✓Tab �
1
2Tgab
◆
We have that:
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
Using the ultrarelativistic equation of state:
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
Using the ultrarelativistic equation of state: p =1
3µ
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
Using the ultrarelativistic equation of state: p =1
3µ
d✓
dt= �µ+
3
2⇠✓ � 2�2 � 1
3✓2
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
Using the ultrarelativistic equation of state: p =1
3µ
d✓
dt= �µ+
3
2⇠✓ � 2�2 � 1
3✓2
We have that:d✓
dt= �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
(After some work!) (See Kohli and Haslam:arXiv:1207.6132v2 [gr-qc])
Using the ultrarelativistic equation of state: p =1
3µ
d✓
dt= �µ+
3
2⇠✓ � 2�2 � 1
3✓2
This is The Raychaudhuri equation with our modification for viscous flow.
The Generalized Friedmann Equation
The Generalized Friedmann Equation
ua;b = ✓ab = Kab
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine:
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine:
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
2.4 The extrinsic curvature 33
δna
δna ∝−Kabna
Figure 2.2 The extrinsic curvature of a hypersurface in an enveloping spacetime measures how much normalvectors to the hypersurface differ at neighboring points. It therefore measures the rate at which the hypersurfacewarps as it is carried forward along a normal vector.
The 3-dimensional covariant derivative can be expressed in terms of 3-dimensionalconnection coefficients, which, in a coordinate basis, are given by
!abc = 1
2γ ad (∂cγdb + ∂bγdc − ∂dγbc). (2.44)
The 3-dimensional Riemann tensor associated with γi j is defined by requiring that8
2D[a Db]wc = Rdcbawd Rd
cband = 0 (2.45)
for any spatial vector wd . In a coordinate basis, the components of the Riemann tensor canbe computed from
R dabc = ∂b!
dac − ∂a!
dbc + !e
ac!deb − !e
bc!dea. (2.46)
Contracting the Riemann tensor yields the 3-dimensional Ricci tensor Rab = Rcacb and the
3-dimensional Ricci scalar R = Raa .
Einstein’s equations (1.32) relate contractions of the 4-dimensional Riemann tensor(4) Ra
bcd to the stress–energy tensor. Since we want to rewrite these equations in terms of3-dimensional objects, we decompose (4) Ra
bcd into spatial tensors. Not surprisingly, thisdecomposition involves its 3-dimensional cousin Ra
bcd , but obviously this cannot containall the information needed. Rd
abc is a purely spatial object and can be computed from spatialderivatives of the spatial metric alone, while (4) Rd
abc is a spacetime creature which alsocontains time derivatives of the 4-dimensional metric. Stated differently, the 3-dimensionalcurvature Ra
bcd only contains information about the curvature intrinsic to a slice $, but itgives no information about what shape this slice takes in the spacetime M in which it isembedded. This information is contained in a tensor called the extrinsic curvature.
2.4 The extrinsic curvature
The extrinsic curvature Kab can be found by projecting gradients of the normal vectorinto the slice $ (see Figure 2.2). We will also see that the extrinsic curvature is related to
8 See equation (1.20) for the 4-dimensional analog of this expression.
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
2.4 The extrinsic curvature 33
δna
δna ∝−Kabna
Figure 2.2 The extrinsic curvature of a hypersurface in an enveloping spacetime measures how much normalvectors to the hypersurface differ at neighboring points. It therefore measures the rate at which the hypersurfacewarps as it is carried forward along a normal vector.
The 3-dimensional covariant derivative can be expressed in terms of 3-dimensionalconnection coefficients, which, in a coordinate basis, are given by
!abc = 1
2γ ad (∂cγdb + ∂bγdc − ∂dγbc). (2.44)
The 3-dimensional Riemann tensor associated with γi j is defined by requiring that8
2D[a Db]wc = Rdcbawd Rd
cband = 0 (2.45)
for any spatial vector wd . In a coordinate basis, the components of the Riemann tensor canbe computed from
R dabc = ∂b!
dac − ∂a!
dbc + !e
ac!deb − !e
bc!dea. (2.46)
Contracting the Riemann tensor yields the 3-dimensional Ricci tensor Rab = Rcacb and the
3-dimensional Ricci scalar R = Raa .
Einstein’s equations (1.32) relate contractions of the 4-dimensional Riemann tensor(4) Ra
bcd to the stress–energy tensor. Since we want to rewrite these equations in terms of3-dimensional objects, we decompose (4) Ra
bcd into spatial tensors. Not surprisingly, thisdecomposition involves its 3-dimensional cousin Ra
bcd , but obviously this cannot containall the information needed. Rd
abc is a purely spatial object and can be computed from spatialderivatives of the spatial metric alone, while (4) Rd
abc is a spacetime creature which alsocontains time derivatives of the 4-dimensional metric. Stated differently, the 3-dimensionalcurvature Ra
bcd only contains information about the curvature intrinsic to a slice $, but itgives no information about what shape this slice takes in the spacetime M in which it isembedded. This information is contained in a tensor called the extrinsic curvature.
2.4 The extrinsic curvature
The extrinsic curvature Kab can be found by projecting gradients of the normal vectorinto the slice $ (see Figure 2.2). We will also see that the extrinsic curvature is related to
8 See equation (1.20) for the 4-dimensional analog of this expression.
Recall from differential geometry, the embedding relation:
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
2.4 The extrinsic curvature 33
δna
δna ∝−Kabna
Figure 2.2 The extrinsic curvature of a hypersurface in an enveloping spacetime measures how much normalvectors to the hypersurface differ at neighboring points. It therefore measures the rate at which the hypersurfacewarps as it is carried forward along a normal vector.
The 3-dimensional covariant derivative can be expressed in terms of 3-dimensionalconnection coefficients, which, in a coordinate basis, are given by
!abc = 1
2γ ad (∂cγdb + ∂bγdc − ∂dγbc). (2.44)
The 3-dimensional Riemann tensor associated with γi j is defined by requiring that8
2D[a Db]wc = Rdcbawd Rd
cband = 0 (2.45)
for any spatial vector wd . In a coordinate basis, the components of the Riemann tensor canbe computed from
R dabc = ∂b!
dac − ∂a!
dbc + !e
ac!deb − !e
bc!dea. (2.46)
Contracting the Riemann tensor yields the 3-dimensional Ricci tensor Rab = Rcacb and the
3-dimensional Ricci scalar R = Raa .
Einstein’s equations (1.32) relate contractions of the 4-dimensional Riemann tensor(4) Ra
bcd to the stress–energy tensor. Since we want to rewrite these equations in terms of3-dimensional objects, we decompose (4) Ra
bcd into spatial tensors. Not surprisingly, thisdecomposition involves its 3-dimensional cousin Ra
bcd , but obviously this cannot containall the information needed. Rd
abc is a purely spatial object and can be computed from spatialderivatives of the spatial metric alone, while (4) Rd
abc is a spacetime creature which alsocontains time derivatives of the 4-dimensional metric. Stated differently, the 3-dimensionalcurvature Ra
bcd only contains information about the curvature intrinsic to a slice $, but itgives no information about what shape this slice takes in the spacetime M in which it isembedded. This information is contained in a tensor called the extrinsic curvature.
2.4 The extrinsic curvature
The extrinsic curvature Kab can be found by projecting gradients of the normal vectorinto the slice $ (see Figure 2.2). We will also see that the extrinsic curvature is related to
8 See equation (1.20) for the 4-dimensional analog of this expression.
Recall from differential geometry, the embedding relation:(4)R =(3) R+K2 �K↵�K↵� � 2(4)R↵�u
↵u�
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
2.4 The extrinsic curvature 33
δna
δna ∝−Kabna
Figure 2.2 The extrinsic curvature of a hypersurface in an enveloping spacetime measures how much normalvectors to the hypersurface differ at neighboring points. It therefore measures the rate at which the hypersurfacewarps as it is carried forward along a normal vector.
The 3-dimensional covariant derivative can be expressed in terms of 3-dimensionalconnection coefficients, which, in a coordinate basis, are given by
!abc = 1
2γ ad (∂cγdb + ∂bγdc − ∂dγbc). (2.44)
The 3-dimensional Riemann tensor associated with γi j is defined by requiring that8
2D[a Db]wc = Rdcbawd Rd
cband = 0 (2.45)
for any spatial vector wd . In a coordinate basis, the components of the Riemann tensor canbe computed from
R dabc = ∂b!
dac − ∂a!
dbc + !e
ac!deb − !e
bc!dea. (2.46)
Contracting the Riemann tensor yields the 3-dimensional Ricci tensor Rab = Rcacb and the
3-dimensional Ricci scalar R = Raa .
Einstein’s equations (1.32) relate contractions of the 4-dimensional Riemann tensor(4) Ra
bcd to the stress–energy tensor. Since we want to rewrite these equations in terms of3-dimensional objects, we decompose (4) Ra
bcd into spatial tensors. Not surprisingly, thisdecomposition involves its 3-dimensional cousin Ra
bcd , but obviously this cannot containall the information needed. Rd
abc is a purely spatial object and can be computed from spatialderivatives of the spatial metric alone, while (4) Rd
abc is a spacetime creature which alsocontains time derivatives of the 4-dimensional metric. Stated differently, the 3-dimensionalcurvature Ra
bcd only contains information about the curvature intrinsic to a slice $, but itgives no information about what shape this slice takes in the spacetime M in which it isembedded. This information is contained in a tensor called the extrinsic curvature.
2.4 The extrinsic curvature
The extrinsic curvature Kab can be found by projecting gradients of the normal vectorinto the slice $ (see Figure 2.2). We will also see that the extrinsic curvature is related to
8 See equation (1.20) for the 4-dimensional analog of this expression.
Recall from differential geometry, the embedding relation:(4)R =(3) R+K2 �K↵�K↵� � 2(4)R↵�u
↵u�
) T↵�u↵� =
1
2
⇣(3)R�K↵�K↵� +K2
⌘
The Generalized Friedmann Equation
ua;b = ✓ab = KabDefine: Extrinsic Curvature tensor: Measure “warping” of spatial slices.
2.4 The extrinsic curvature 33
δna
δna ∝−Kabna
Figure 2.2 The extrinsic curvature of a hypersurface in an enveloping spacetime measures how much normalvectors to the hypersurface differ at neighboring points. It therefore measures the rate at which the hypersurfacewarps as it is carried forward along a normal vector.
The 3-dimensional covariant derivative can be expressed in terms of 3-dimensionalconnection coefficients, which, in a coordinate basis, are given by
!abc = 1
2γ ad (∂cγdb + ∂bγdc − ∂dγbc). (2.44)
The 3-dimensional Riemann tensor associated with γi j is defined by requiring that8
2D[a Db]wc = Rdcbawd Rd
cband = 0 (2.45)
for any spatial vector wd . In a coordinate basis, the components of the Riemann tensor canbe computed from
R dabc = ∂b!
dac − ∂a!
dbc + !e
ac!deb − !e
bc!dea. (2.46)
Contracting the Riemann tensor yields the 3-dimensional Ricci tensor Rab = Rcacb and the
3-dimensional Ricci scalar R = Raa .
Einstein’s equations (1.32) relate contractions of the 4-dimensional Riemann tensor(4) Ra
bcd to the stress–energy tensor. Since we want to rewrite these equations in terms of3-dimensional objects, we decompose (4) Ra
bcd into spatial tensors. Not surprisingly, thisdecomposition involves its 3-dimensional cousin Ra
bcd , but obviously this cannot containall the information needed. Rd
abc is a purely spatial object and can be computed from spatialderivatives of the spatial metric alone, while (4) Rd
abc is a spacetime creature which alsocontains time derivatives of the 4-dimensional metric. Stated differently, the 3-dimensionalcurvature Ra
bcd only contains information about the curvature intrinsic to a slice $, but itgives no information about what shape this slice takes in the spacetime M in which it isembedded. This information is contained in a tensor called the extrinsic curvature.
2.4 The extrinsic curvature
The extrinsic curvature Kab can be found by projecting gradients of the normal vectorinto the slice $ (see Figure 2.2). We will also see that the extrinsic curvature is related to
8 See equation (1.20) for the 4-dimensional analog of this expression.
Recall from differential geometry, the embedding relation:(4)R =(3) R+K2 �K↵�K↵� � 2(4)R↵�u
↵u�
) T↵�u↵� =
1
2
⇣(3)R�K↵�K↵� +K2
⌘
(From Baumgarte et.al. - “Numerical Relativity”)
Upon applying the decomposition equation, we get (after some work!):
Upon applying the decomposition equation, we get (after some work!):
1
3✓2 =
1
2�ab�
ab � 1
2
(3)
R+ µ
Upon applying the decomposition equation, we get (after some work!):
1
3✓2 =
1
2�ab�
ab � 1
2
(3)
R+ µ
Upon applying the decomposition equation, we get (after some work!):
1
3✓2 =
1
2�ab�
ab � 1
2
(3)
R+ µ
This is The Generalized Friedmann Equation.
The Shear Propagation Equations
The Shear Propagation Equations
Describe the evolution of the anisotropy in a cosmological model as a function of time.
The Shear Propagation Equations
Describe the evolution of the anisotropy in a cosmological model as a function of time.
Derivation is time-consuming!
The Shear Propagation Equations
Describe the evolution of the anisotropy in a cosmological model as a function of time.
Derivation is time-consuming!
The interested reader is encouraged to consult the texts by: Ellis and Wainwright, Hervik and Gron, or Plebanski.
The shear propagation equations are given as:
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:(3)Rab = �✏cda nbcad � ✏cdb nacad + 2nadn
db � nnab � �ab
✓2a2 + ncdn
cd � 1
2n2
◆
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:(3)Rab = �✏cda nbcad � ✏cdb nacad + 2nadn
db � nnab � �ab
✓2a2 + ncdn
cd � 1
2n2
◆
Ricci scalar:
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:(3)Rab = �✏cda nbcad � ✏cdb nacad + 2nadn
db � nnab � �ab
✓2a2 + ncdn
cd � 1
2n2
◆
Ricci scalar:(3)R =(3) Ra
a = �✓6a2 + ncdn
cd � 1
2n2
◆
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:(3)Rab = �✏cda nbcad � ✏cdb nacad + 2nadn
db � nnab � �ab
✓2a2 + ncdn
cd � 1
2n2
◆
Ricci scalar:(3)R =(3) Ra
a = �✓6a2 + ncdn
cd � 1
2n2
◆
But, at the expense of some constraint equations:
The shear propagation equations are given as:
˙�ab + ✓�ab � �da✏bcd⌦
c � �db ✏acd⌦
c +(3) Rab �1
3�(3)ab R = 2⌘�ab
The beauty of the orthonormal frame approach is that the Ricci tensor is now expressed in canonical
coordinate-free form:(3)Rab = �✏cda nbcad � ✏cdb nacad + 2nadn
db � nnab � �ab
✓2a2 + ncdn
cd � 1
2n2
◆
Ricci scalar:(3)R =(3) Ra
a = �✓6a2 + ncdn
cd � 1
2n2
◆
But, at the expense of some constraint equations:3a�33 +
�n11 � n22
��21 = 0
3a�31 + n22�32 = 0
3a�32 � n11�31 = 0
Applying this set of equations to The Bianchi Type IV model:
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0These restrict the form of the shear tensor (symmetric
and traceless):
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0These restrict the form of the shear tensor (symmetric
and traceless):For the diagonal components (a = b):
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0These restrict the form of the shear tensor (symmetric
and traceless):For the diagonal components (a = b):
�ab =⇣�+ +
p3��,�+ �
p3��,�2�+
⌘
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0These restrict the form of the shear tensor (symmetric
and traceless):For the diagonal components (a = b):
�ab =⇣�+ +
p3��,�+ �
p3��,�2�+
⌘
For the off-diagonal components:
Applying this set of equations to The Bianchi Type IV model:
n11 = N, and n22 = n33 = 0, where N > 0
The constraint equations give:
3a�33 +N�21 = 0
3a�31 = 0
3a�32 � �31 = 0These restrict the form of the shear tensor (symmetric
and traceless):For the diagonal components (a = b):
�ab =⇣�+ +
p3��,�+ �
p3��,�2�+
⌘
For the off-diagonal components:
�21 = �12 =�3a�33
N=
6a�+
N
With this shear tensor, the shear propagation equations become:
With this shear tensor, the shear propagation equations become:
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
With this shear tensor, the shear propagation equations become:
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
�+ = �N2
6� �+✓
5+ 2⌘�+
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
µ = �12a2⌘ � 4µ⌘ � ⌘N2 � 4µ✓
3+
4⌘✓2
3+ ✓2⇠
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
µ = �12a2⌘ � 4µ⌘ � ⌘N2 � 4µ✓
3+
4⌘✓2
3+ ✓2⇠
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
µ = �12a2⌘ � 4µ⌘ � ⌘N2 � 4µ✓
3+
4⌘✓2
3+ ✓2⇠
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
�+ = �N2
6� �+✓
5+ 2⌘�+
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
µ = �12a2⌘ � 4µ⌘ � ⌘N2 � 4µ✓
3+
4⌘✓2
3+ ✓2⇠
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
�+ = �N2
6� �+✓
5+ 2⌘�+
a = �a
✓✓
3� 2�+
◆
We have therefore reduced The Einstein Field equations for The Bianchi Type-IV model to a system of first-
order ordinary differential equations!
✓ =1
2
�12a2 + 2µ+N2 � 2✓2 + 3✓⇠
�
µ = �12a2⌘ � 4µ⌘ � ⌘N2 � 4µ✓
3+
4⌘✓2
3+ ✓2⇠
�� = � N2
2p3+
24p3a2�2
+
N2� ��✓ + 2��⌘
�+ = �N2
6� �+✓
5+ 2⌘�+
a = �a
✓✓
3� 2�+
◆
N = N
✓
3+ 2
⇣�+ +
p3��
⌘�
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar:
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
s
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:H = �(1 + q)H2
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:H = �(1 + q)H2
s = s0e⌧
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:H = �(1 + q)H2
s = s0e⌧ A dimensionless time variable
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:H = �(1 + q)H2
s = s0e⌧ A dimensionless time variable
We can show that:
This six-dimensional system has no exact solution, so numerical methods must be employed. However, we can
simplify the system of equations, by re-writing it in Expansion-Normalized Form:
Define the quantities:
✓ ⌘ 3H where, H is the Hubble scalar: H =s
sq = � ss
s2A deceleration parameter
Clearly:H = �(1 + q)H2
s = s0e⌧ A dimensionless time variable
We can show that:dt
d⌧=
1
H) dH
d⌧⌘ H 0 = �(1 + q)H
Define the additional quantities:
Define the additional quantities:
Normalized density parameter
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
) q = ⌦� ⇠
H� 2⌃2
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
) q = ⌦� ⇠
H� 2⌃2
In addition:
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
) q = ⌦� ⇠
H� 2⌃2
In addition:⇠
H= 3⇠0,
⌘
H= 3⌘0, where ⇠0, ⌘0 > 0
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
) q = ⌦� ⇠
H� 2⌃2
In addition:⇠
H= 3⇠0,
⌘
H= 3⌘0, where ⇠0, ⌘0 > 0, n =
N
H,A =
a
H,⌃± =
�±H
Define the additional quantities:
Normalized density parameter
⌃2 =�2
3H2Normalized shear parameter
K = �(3)R
6H2Normalized scalar curvature
By comparing the two expansion-rate equations, we have:
�(1 + q)H2 = �1
3µ+ ⇠H � 2
3�2 �H2
) q = ⌦� ⇠
H� 2⌃2
In addition:⇠
H= 3⇠0,
⌘
H= 3⌘0, where ⇠0, ⌘0 > 0, n =
N
H,A =
a
H,⌃± =
�±H
⌦ =µ
3H2� 0
By making these substitutions, the dynamical system takes the 5-D form:
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
Where:
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
Where:q = ⌦� 3⇠0 � 2⌃2,
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
Where:q = ⌦� 3⇠0 � 2⌃2, ⌃2 = ⌃2
+ + ⌃2�,
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
Where:q = ⌦� 3⇠0 � 2⌃2, ⌃2 = ⌃2
+ + ⌃2�, ⌦ � 0
By making these substitutions, the dynamical system takes the 5-D form:
⌃0� = � n2
2p3+ 24
p3A2⌃2
+
n2� 3⌃� � 6⌃�⌘0 + (1 + q)⌃�
⌃0+ = �1
6n2 � 3
5⌃+ + 6⌘0⌃+ + (1 + q)⌃+
A0 = �A+ 2⌃+A+ (1 + q)A
n0 = n+ 2n⇣⌃+ +
p3⌃�
⌘+ (1 + q)n
⌦0 = ⌘0��12A2 � 12⌦� n2
�� 4⌦+ 12⌘0 + 9⇠0 + 2⌦(1 + q)
Where:q = ⌦� 3⇠0 � 2⌃2, ⌃2 = ⌃2
+ + ⌃2�, ⌦ � 0
The expansion variable is now decoupled from the system of equations, with the “cost” of assuming expansion.
Solutions of The Dynamical System
Solutions of The Dynamical System
In our numerical experiments, we expect the following reasonable results:
The models should become asymptotic to a FLRW model with vanishing anisotropy
The energy density should decrease as the universe model expands
Which values of the viscosity parameters lead to these results?
Solutions of The Dynamical System
In our numerical experiments, we expect the following reasonable results:
The models should become asymptotic to a FLRW model with vanishing anisotropy
The energy density should decrease as the universe model expands
Which values of the viscosity parameters lead to these results?
⇠0, ⌘0
A Note on The Singularity Theorem
Recall The Raychaudhuri Equation:
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
) �1
2 (µ+ 3p) +
3
2⇠✓ 0
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
) �1
2 (µ+ 3p) +
3
2⇠✓ 0
Assuming The Equation of State:
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
) �1
2 (µ+ 3p) +
3
2⇠✓ 0
Assuming The Equation of State:
⇠ =C
✓, C 2 R+
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
) �1
2 (µ+ 3p) +
3
2⇠✓ 0
Assuming The Equation of State:
⇠ =C
✓, C 2 R+
) ✓ +1
2 (µ+ 3p)� 3
2C +
1
3✓2 = �2�2 0
Recall The Raychaudhuri Equation:
✓ = �1
2 (µ+ 3p) +
3
2⇠✓ � 2�2 � 1
3✓2
And The SEC:Rabuaub � 0
) �1
2 (µ+ 3p) +
3
2⇠✓ 0
Assuming The Equation of State:
⇠ =C
✓, C 2 R+
) ✓ +1
2 (µ+ 3p)� 3
2C +
1
3✓2 = �2�2 0
) ✓ +1
3✓2 0
) ✓ �1
3✓2
Assuming a Strict Inequality:
Assuming a Strict Inequality:
) 1
✓(t) 1
✓i+
t
3
Assuming a Strict Inequality:
) 1
✓(t) 1
✓i+
t
3
) 8 t 2 R, 9 tsing such that:1
✓(tsing)= 0
Assuming a Strict Inequality:
) 1
✓(t) 1
✓i+
t
3
) 8 t 2 R, 9 tsing such that:1
✓(tsing)= 0
) 1
✓(tsing)= 0 ) ✓(tsing) = 1
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define:
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define: d = sup{h : F (t) < 0 on [a, h)}
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define: d = sup{h : F (t) < 0 on [a, h)}Clearly:
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define: d = sup{h : F (t) < 0 on [a, h)}Clearly: d b
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define: d = sup{h : F (t) < 0 on [a, h)}Clearly: d b
One cannot have F (d) > 0, since this would mean that F > 0 on someinterval to the left of d.
Assuming a strict equality, one can employ the IVT to prove the existence of a singularity point:
F (t) ⌘ 1
✓(t)=
1
✓i+
t
3
Lemma:Let F (t) ⌘ 1
✓(t) =1✓i+
t3 be continuous on [a,b]. If F (a) < 0 < F (b)_F (b) <
0 < F (a) ) 9 d, such that a < d < b for which F (d) = 0.
“Proof:”Suppose that F (a) < 0 < F (b). Since F (a) < 0, by the continuity of F (t),
9 h 2 R such that F < 0 on [a, h).
Define: d = sup{h : F (t) < 0 on [a, h)}Clearly: d b
One cannot have F (d) > 0, since this would mean that F > 0 on someinterval to the left of d.CONTRADICTION!
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!Therefore, it must be that F (d) = 0.
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!Therefore, it must be that F (d) = 0.
Therefore, this model of the universe emerged from an initial singularity point.
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!Therefore, it must be that F (d) = 0.
Therefore, this model of the universe emerged from an initial singularity point.
This has been a demonstration of the famous Penrose-Hawking Singularity Theorem:
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!Therefore, it must be that F (d) = 0.
Therefore, this model of the universe emerged from an initial singularity point.
This has been a demonstration of the famous Penrose-Hawking Singularity Theorem:
We also cannot have F (d) < 0, since this would imply that there would be
an interval [a, t), with t > d which would in turn imply that F (t) < 0
CONTRADICTION!Therefore, it must be that F (d) = 0.
Therefore, this model of the universe emerged from an initial singularity point.
This has been a demonstration of the famous Penrose-Hawking Singularity Theorem:
More or less, we can say that if matter as described by the energy-momentum
tensor satisfies the strong energy condition, and there exists a
↵ 2 R+such that ✓(t) > ↵,
everywhere in the past of a specific spatial slice, then, there exists a singularity
point where all geodesics end.
THE END!