Intro to Matrix Analysis
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Transcript of Intro to Matrix Analysis
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Engineering Systems
Lumped Parameter
(Discrete)Continuous
• A finite number ofstate variablesdescribe solution
• Algebraic Equations
• Differential EquationsGovern Response
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Lumped Parameter
Displacements of Joints fully describe sDisplacements of Joints fully describe s
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Matrix Structural Analysis - Objectives
Use
Equations of Equilibrium
Constitutive Equations
Compatibility Conditions
Basic Equations
Form
[A]{x}={b}
Solve for Unno!n "ispla#ements$For#es
{x}= [A]%&{b}
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Terminology
Element:Discrete StructuralMemberodes:Characteristicpoints that deneelement!"O"#":
All possibledirections ofdisplacements @ anode
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Assumptions
• 'inear Strain%"ispla#ement (elations)ip
• Small "eformations
• Equilibrium *ertains to Undeformed Confi+uration
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T$e Sti%%ness Met$od
&onsider a simple spring structural member
Undeformed Configuration
Deformed Configuration
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
1
2
*1
*2
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
2
=
1+
For each case write basic equations
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
2=0 1
P11 P21
X
Equilibrium
21112111 0 P P P P −=⇒=+Constitutive
111 δ k P =
P11
121 δ k P −=111 δ k P =
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
2
1=0
P12P22
Equilibrium
12222212 0 P P P P −=⇒=+Constitutive
222 δ k P =
212 δ k P −=222 δ k P =
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
Combined Action
P1P2
2112111 δ δ k k P P P −=+=
2122212 δ δ k k P P P +−=+=
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!erivation o% Sti%%ness Matrix 'sing (asicE)uations
In atri! Form
2112111 δ δ k k P P P −=+=
2122212 δ δ k k P P P +−=+=
−
−
=
2
1
2
1
δ
δ
k k
k k
P
P
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&onsider * Springs
2 elements 3 nodes 3 dof
1
Fix Fix
2
Fix Fix
3
Fix Fix
+ * ,
+ *
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*-Springs
=
−
+−
−
3
2
1
3
2
1
22
2
2
1
1
11
0
0
P
P P
k k
k k
k k
k k
δ
δ δ
&ompare to +-Spring
=
−
−2
1
2
1
11
11
P
P
k k
k k
δ
δ
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Properties o% Sti%%ness Matrix
SM is Symmetric(etti-Max.ell La.
SM is Singularo (oundary &onditions Applied /et
Main !iagonal o% SM Positiveecessary %or Stability
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Apply (oundary &onditions
k ii k ij k ik k il k im uiu j
uk
ul
k ji k jj k jk k jl k jm
k ki k kj k kk k kl k km
k li k lj k lk k ll k lm
k li k lj k lk k ll k lm um
!i! j
!k
!l
!m
" ##
" #s
" s# " ss
u#
P#
us Ps
" ff uf " " fsusPf
" sf uf " " ssusPs " sf uf " " ssusPs
uf " ff #Pf " " fsus$$1
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Trans%ormations
P
k 2k 1
δ1
δ2
δ3
δ2
u1
u2
u3
u%
u3
u%
u&
u'
x
(Global C$
xLocal C$
b&ective' ransform $tate ariables from LC$ to GC$
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Trans%ormations
Consider
P*"
P*+
P*+ , P*+cosφ + P*"sinφ
P*" , -P*+sinφ + P*"cosφ
P*+
P*",
cosφ sinφ
-sinφ cosφ
P*+
P*"
P* , P*
x
(Global C$
φ
P*+
P.+
.
P."
*
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Trans%ormations
/n General/n General
P*"
P*+ P* , P*
x
(Global C$
φ
P*+
P.+
.
P."
*
P. , P.
u. , u.
u* , u*
$imilarl" for u$imilarl " for u
P* , P*-*
or
P. , P.-*
or
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Trans%ormationsElement stiffness equations in Local C$
0 ,* -*
-* *
δ*δ.
P*
P.
E+pand to 1 Local dof
0
* # -* ## # # #-* # * ## # # #
u*+u*"
u.+u."
,
P*+P*"
P.+P."
P*+
P.+P."
P*"
φ
.
*
P*
P.
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SM in 0lobal &oordinate System
/ntroduce t2e transformed variables3
4 u , PRR-*
4 ' Element $% in global C$
56 5#6
5#6 565R6,7ot2 R and Depend on Particular Element
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Trans%ormations
!or e+ample for an a+ial element 8it2 0,AE9L
AE9L
l. lm - l. - lm
$"mm:
m. - lm - m.
l. lmm.
4 ,
l,cosφ m,sinφ
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1n Summary
• !erivation o% element SM 2 (asicE)uations
• Structural SM by Superposition
• Application o% (oundary &onditions -
Elimination
• Solution o% Sti%%ness E)uations 2
Partitioning
• Local 3 0lobal &S
• Trans%ormation