Topic 1 Surface Resistance Part II
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Transcript of Topic 1 Surface Resistance Part II
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Surface Resistance
Part II
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Fully Developed Flow between Parallel
Plates Using the Navier-Stokes Equations
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Navier-Stokes Equations without Body Forces
( ) ( ) ( )Continuity: 0
u v w
t x y z
+ + + =
( ) ( ) ( ) ( )2 1x-momentum:
Re
xyxx xzuu uv uw p
t x y z x x y z
+ + + = + + +
( ) ( ) ( ) ( )2 1y-momentum:
Re
xy yy yzvv uv vw p
t x y z y x y z
+ + + = + + +
( ) ( ) ( ) ( )2 1z-momentum:
Re
yzxz zzww uw vw p
t x y z z x y z
+ + + = + + +
( ) ( ) ( ) ( ) ( ) ( ) ( )
( ) ( ) ( )
Energy:
1
RePr
1
Re
T T T T
yx z
xx xy xz xy yy yz xz yz zz
E uE vE wE up vp wp
t x y z x y z
qq q
x y z
u v w u v w u v wx y z
+ + + =
+ + +
+ + + + + + + + +
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Fully Developed Flow between Parallel Plates Using
the Navier-Stokes Equations
The governing equation for laminar flow over a surface can also be
derived using the Navier-Stokes equations.
Introduce the new variables xis the coordinate in the direction of
flo
w (same as s)and y perpendicular to the plates.
x
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Fully Developed Flow between Parallel Plates Using
the Navier-Stokes Equations
The flow field is fully developed, so the derivatives
Also the flow is steady, so
The components of the gravity force are
The continuity equation is
Therefore
Continuity equation is automatically satisfied!
0u
x
=
0
v
x
=
0v
t
=
-direction sinx g
u
x
0
v
y
+ =
0 constant 0v
v vy
= = =
0u
t
=
-direction cosy g
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Fully Developed Flow between Parallel Plates Using
the Navier-Stokes Equations
Momentum equation in the y direction is
As v is zero everywhere, there is no acceleration of the fluid in
the y direction and equation reduces to
By integrating last equation we can get
where py=0(x) is the pressure distribution along the lower wall.We can see that pressure is decreasing with the elevation in
the duct.
We can rewrite this equation as
where
v
t
vux
vvy
2
2
p v(y x
2
2
v
y
) g cos
cosgyp =
)(cos 0 xpygp y=+=
)(0 xpzp y==+
zy =cos
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Fully Developed Flow between Parallel Plates Using
the Navier-Stokes Equations
The gradient of pressure in the x direction is
Momentum equation in the x direction is
For steady, fully developed flow all the terms in the left-handside of the equation equal zero and the equation becomes
As u is a function ofy and is function of x only we can
rewrite this equation in this form
As the slope is
We can rewrite the last equation as
u
t
uu
x
+
v+
2
2(
u p u
y x x
= +
2
2) sin
ug
y
+ +
dx
dp
dx
dp
x
p y==
=0
2
2
siny
upg
x
p
=
xp /
2
2
sindy
udgdxdp =
dx
dz=sin
2
2
)(dy
udzp
dx
d =+
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Fully Developed Flow between Parallel Plates Using
the Navier-Stokes Equations
2
2
d d up zdx dy
)(12
2
zpds
d
dy
ud
+=From SimpleForce Balance
From N-S
Equations
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Surface Resistance
Solution of Laminar Boundary
Layer by Blasius
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Surface Resistance
Turbulent Velocity Profile
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Turbulent
Boundary
Layer
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Surface Resistance
Shear Stress at Turbulent Region
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Boundary Layer
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Boundary Layer