Exercise 041515

20
MEMBER ab LOCAL - ELE Notation for Node 1 a Notation for Node 2 b ua va Fxa = 120 0 AREA AND GEOMETRIC PROPERTIES Fya 0 0.48 Length (mm) 10000 L Mza 0 2400 Area (mm^2) 6000 A Fxb -120 0 Iy (mm^4) 0 Iy Fyb 0 -0.48 Iz (mm^4) 200000000 Iz Mzb 0 2400 J (mm^4) 300000000 J E (GPa) 200 E TRANS G (GPa) 76.923076923077 G v 0.3 v Fxa Fya Fx'a = 0.000000 1.000000 Local : x', y', z' Global: x, y, z Fy'a -1.000000 0.000000 x to x' 90 Mz'a 0.000000 0.000000 y to x' 0 Fx'b 0.000000 0.000000 x to y' 180 Fy'b 0.000000 0.000000 y to y' 90 Mz'b 0.000000 0.000000 ua va Fxa = 7.351E-15 -0.48 Fya 120 2.94E-17 Mza 0 2400 Fxb -7.35E-15 0.48 Fyb -120 -2.94E-17 Mzb 0 2400 ua va Fxa 0 0 Fya 0 120 Mza -2400 0 Fxb 0 0 Fyb 0 -120 Mzb -2400 0 αx βx αy βy [K]

description

8

Transcript of Exercise 041515

Page 1: Exercise 041515

MEMBER ab LOCAL - ELEMENT STIFFNESS MATRIX [K']Notation for Node 1 a

Notation for Node 2 b ua va θza

Fxa

=

120 0 0

AREA AND GEOMETRIC PROPERTIES Fya 0 0.48 2400

Length (mm) 10000 L Mza 0 2400 16000000

Area (mm^2) 6000 A Fxb -120 0 0

Iy (mm^4) 0 Iy Fyb 0 -0.48 -2400

Iz (mm^4) 200000000 Iz Mzb 0 2400 8000000

J (mm^4) 300000000 J

E (GPa) 200 E TRANSFORMATION MATRIX [Γ]G (GPa) 76.9230769230769 G

v 0.3 v Fxa Fya Mza

Fx'a

=

0.000000 1.000000 0.000000

Local : x', y', z' Global: x, y, z Fy'a -1.000000 0.000000 0.000000

x to x' 90 Mz'a 0.000000 0.000000 1.000000

y to x' 0 Fx'b 0.000000 0.000000 0.000000

x to y' 180 Fy'b 0.000000 0.000000 0.000000

y to y' 90 Mz'b 0.000000 0.000000 0.000000

ua va θza

Fxa

=

7.3509E-15 -0.48 -2400

Fya 120 2.9404E-17 1.4702E-13

Mza 0 2400 16000000

Fxb -7.3509E-15 0.48 2400

Fyb -120 -2.9404E-17 -1.4702E-13

Mzb 0 2400 8000000

[K] - FOR GLOBAL

ua va θza

Fxa 0 0 -2400

Fya 0 120 0

Mza -2400 0 16000000

Fxb 0 0 2400

Fyb 0 -120 0

Mzb -2400 0 8000000

αx

βx

αy

βy

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 2: Exercise 041515

LOCAL - ELEMENT STIFFNESS MATRIX [K']

ub vb θzb

-120 0 0 ua

0 -0.48 2400 va

0 -2400 8000000 θza

120 0 0 ub

0 0.48 -2400 vb

0 -2400 16000000 θzb

TRANSFORMATION MATRIX [Γ]

Fxb Fyb Mzb

0.000000 0.000000 0.000000 Fxa

0.000000 0.000000 0.000000 Fya

0.000000 0.000000 0.000000 Mza

0.000000 1.000000 0.000000 Fxb

-1.000000 0.000000 0.000000 Fyb

0.000000 0.000000 1.000000 Mzb

ub vb θzb

-7.3509E-15 0.48 -2400 ua

-120 -2.9404E-17 1.4702E-13 va

0 -2400 8000000 θza

7.3509E-15 -0.48 2400 ub

120 2.9404E-17 -1.4702E-13 vb

0 -2400 16000000 θzb

[K] - FOR GLOBAL

ub vb θzb

0 0 -2400 ua

0 -120 0 va

2400 0 8000000 θza

0 0 2400 ub

0 120 0 vb

2400 0 16000000 θzb

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 3: Exercise 041515

MEMBER bc LOCAL - ELEMENT STIFFNESS MATRIX [K']Notation for Node 1 b

Notation for Node 2 c ub vb θzb

Fxb

=

75 0 0

AREA AND GEOMETRIC PROPERTIES Fyb 0 0.234375 937.5

Length (mm) 8000 L Mzb 0 937.5 5000000

Area (mm^2) 3000 A Fxc -75 0 0

Iy (mm^4) 0 Iy Fyc 0 -0.234375 -937.5

Iz (mm^4) 50000000 Iz Mzc 0 937.5 2500000

J (mm^4) 70000000 J

E (GPa) 200 E TRANSFORMATION MATRIX [Γ]G (GPa) 76.9230769230769 G

v 0.3 v Fxb Fyb Mzb

Fx'b

=

1.000000 0.000000 0.000000

Local : x', y', z' Global: x, y, z Fy'b 0.000000 1.000000 0.000000

x to x' 0 Mz'b 0.000000 0.000000 1.000000

y to x' 90 Fx'c 0.000000 0.000000 0.000000

x to y' 90 Fy'c 0.000000 0.000000 0.000000

y to y' 0 Mz'c 0.000000 0.000000 0.000000

ub vb θzb

Fxb

=

75 1.4357E-17 5.7429E-14

Fyb 4.5943E-15 0.234375 937.5

Mzb 0 937.5 5000000

Fxc -75 -1.4357E-17 -5.7429E-14

Fyc -4.5943E-15 -0.234375 -937.5

Mzc 0 937.5 2500000

[K] - FOR GLOBAL

ub vb θzb

Fxb 75 4.6087E-15 5.7429E-14

Fyb 4.6087E-15 0.234375 937.5

Mzb 5.7429E-14 937.5 5000000

Fxc -75 -4.6087E-15 -5.7429E-14

Fyc -4.6087E-15 -0.234375 -937.5

Mzc 5.7429E-14 937.5 2500000

αx

βx

αy

βy

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 4: Exercise 041515

LOCAL - ELEMENT STIFFNESS MATRIX [K']

uc vc θzc

-75 0 0 ub

0 -0.234375 937.5 vb

0 -937.5 2500000 θzb

75 0 0 uc

0 0.234375 -937.5 vc

0 -937.5 5000000 θzc

TRANSFORMATION MATRIX [Γ]

Fxc Fyc Mzc

0.000000 0.000000 0.000000 Fxb

0.000000 0.000000 0.000000 Fyb

0.000000 0.000000 0.000000 Mzb

1.000000 0.000000 0.000000 Fxc

0.000000 1.000000 0.000000 Fyc

0.000000 0.000000 1.000000 Mzc

uc vc θzc

-75 -1.4357E-17 5.7429E-14 ub

-4.5943E-15 -0.234375 937.5 vb

0 -937.5 2500000 θzb

75 1.4357E-17 -5.7429E-14 uc

4.5943E-15 0.234375 -937.5 vc

0 -937.5 5000000 θzc

[K] - FOR GLOBAL

uc vc θzc

-75 -4.6087E-15 5.7429E-14 ub

-4.6087E-15 -0.234375 937.5 vb

-5.7429E-14 -937.5 2500000 θzb

75 4.6087E-15 -5.7429E-14 uc

4.6087E-15 0.234375 -937.5 vc

-5.7429E-14 -937.5 5000000 θzc

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 5: Exercise 041515

MEMBER cd LOCAL - ELEMENT STIFFNESS MATRIX [K']Notation for Node 1 c

Notation for Node 2 d uc vc θzc

Fxc

=

120 0 0

AREA AND GEOMETRIC PROPERTIES Fyc 0 0.48 2400

Length (mm) 10000 L Mzc 0 2400 16000000

Area (mm^2) 6000 A Fxd -120 0 0

Iy (mm^4) 0 Iy Fyd 0 -0.48 -2400

Iz (mm^4) 200000000 Iz Mzd 0 2400 8000000

J (mm^4) 300000000 J

E (GPa) 200 E TRANSFORMATION MATRIX [Γ]G (GPa) 76.9230769230769 G

v 0.3 v Fxc Fyc Mzc

Fx'c

=

0.000000 -1.000000 0.000000

Local : x', y', z' Global: x, y, z Fy'c 1.000000 0.000000 0.000000

x to x' 270 Mz'c 0.000000 0.000000 1.000000

y to x' 180 Fx'd 0.000000 0.000000 0.000000

x to y' 0 Fy'd 0.000000 0.000000 0.000000

y to y' 270 Mz'd 0.000000 0.000000 0.000000

uc vc θzc

Fxc

=

-2.2053E-14 0.48 2400

Fyc -120 -8.8211E-17 -4.4105E-13

Mzc 0 2400 16000000

Fxd 2.2053E-14 -0.48 -2400

Fyd 120 8.8211E-17 4.4105E-13

Mzd 0 2400 8000000

[K] - FOR GLOBAL

uc vc θzc

Fxc 0.48 2.1964E-14 2400

Fyc 2.1964E-14 120 -4.4105E-13

Mzc 2400 -4.4105E-13 16000000

Fxd -0.48 -2.1964E-14 -2400

Fyd -2.1964E-14 -120 4.4105E-13

Mzd 2400 -4.4105E-13 8000000

αx

βx

αy

βy

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 6: Exercise 041515

LOCAL - ELEMENT STIFFNESS MATRIX [K']

ud vd θzd

-120 0 0 uc

0 -0.48 2400 vc

0 -2400 8000000 θzc

120 0 0 ud

0 0.48 -2400 vd

0 -2400 16000000 θzd

TRANSFORMATION MATRIX [Γ]

Fxd Fyd Mzd

0.000000 0.000000 0.000000 Fxc

0.000000 0.000000 0.000000 Fyc

0.000000 0.000000 0.000000 Mzc

0.000000 -1.000000 0.000000 Fxd

1.000000 0.000000 0.000000 Fyd

0.000000 0.000000 1.000000 Mzd

ud vd θzd

2.2053E-14 -0.48 2400 uc

120 8.8211E-17 -4.4105E-13 vc

0 -2400 8000000 θzc

-2.2053E-14 0.48 -2400 ud

-120 -8.8211E-17 4.4105E-13 vd

0 -2400 16000000 θzd

[K] - FOR GLOBAL

ud vd θzd

-0.48 -2.1964E-14 2400 uc

-2.1964E-14 -120 -4.4105E-13 vc

-2400 4.4105E-13 8000000 θzc

0.48 2.1964E-14 -2400 ud

2.1964E-14 120 4.4105E-13 vd

-2400 4.4105E-13 16000000 θzd

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 7: Exercise 041515

MEMBER ac LOCAL - ELEMENT STIFFNESS MATRIX [K']Notation for Node 1 a

Notation for Node 2 c ua va θza

Fxa

=

46.8521286 0 0

AREA AND GEOMETRIC PROPERTIES Fya 0 0.05713674 365.853659

Length (mm) 12806.24847 L Mza 0 365.853659 3123475.24

Area (mm^2) 3000 A Fxc -46.8521286 0 0

Iy (mm^4) 0 Iy Fyc 0 -0.05713674 -365.853659

Iz (mm^4) 50000000 Iz Mzc 0 365.853659 1561737.62

J (mm^4) 70000000 J

E (GPa) 200 E TRANSFORMATION MATRIX [Γ]G (GPa) 76.9230769230769 G

v 0.3 v Fxa Fya Mza

Fx'a

=

0.624695 0.780869 0.000000

Local : x', y', z' Global: x, y, z Fy'a -0.780869 0.624695 0.000000

x to x' 51.34019175 Mz'a 0.000000 0.000000 1.000000

y to x' 321.34019175 Fx'c 0.000000 0.000000 0.000000

x to y' 141.34019175 Fy'c 0.000000 0.000000 0.000000

y to y' 51.34019175 Mz'c 0.000000 0.000000 0.000000

ua va θza

Fxa

=

29.2682927 -0.0446163 -285.683711

Fya 36.5853659 0.03569304 228.546969

Mza 0 365.853659 3123475.24

Fxc -29.2682927 0.0446163 285.683711

Fyc -36.5853659 -0.03569304 -228.546969

Mzc 0 365.853659 1561737.62

[K] - FOR GLOBAL

ua va θza

Fxa 18.318597 22.8268253 -285.683711

Fya 22.8268253 28.5906684 228.546969

Mza -285.683711 228.546969 3123475.24

Fxc -18.318597 -22.8268253 285.683711

Fyc -22.8268253 -28.5906684 -228.546969

Mzc -285.683711 228.546969 1561737.62

αx

βx

αy

βy

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 8: Exercise 041515

LOCAL - ELEMENT STIFFNESS MATRIX [K']

uc vc θzc

-46.8521286 0 0 ua

0 -0.05713674 365.853659 va

0 -365.853659 1561737.62 θza

46.8521286 0 0 uc

0 0.05713674 -365.853659 vc

0 -365.853659 3123475.24 θzc

TRANSFORMATION MATRIX [Γ]

Fxc Fyc Mzc

0.000000 0.000000 0.000000 Fxa

0.000000 0.000000 0.000000 Fya

0.000000 0.000000 0.000000 Mza

0.624695 0.780869 0.000000 Fxc

-0.780869 0.624695 0.000000 Fyc

0.000000 0.000000 1.000000 Mzc

uc vc θzc

-29.2682927 0.0446163 -285.683711 ua

-36.5853659 -0.03569304 228.546969 va

0 -365.853659 1561737.62 θza

29.2682927 -0.0446163 285.683711 uc

36.5853659 0.03569304 -228.546969 vc

0 -365.853659 3123475.24 θzc

[K] - FOR GLOBAL

uc vc θzc

-18.318597 -22.8268253 -285.683711 ua

-22.8268253 -28.5906684 228.546969 va

285.683711 -228.546969 1561737.62 θza

18.318597 22.8268253 285.683711 uc

22.8268253 28.5906684 -228.546969 vc

285.683711 -228.546969 3123475.24 θzc

[Γ]T * [K']

[K] = [Γ]T * [K'] * [Γ]

Page 9: Exercise 041515

GLOBAL STIFFNESS MATRIXNODE NOTATIONS

Node 1 a

Node 2 b ua va θza ub vb

Node 3 c Fxa

=

19 23 -2686 0 0

Node 4 d Fya 23 149 229 0 -120

Node 5 Mza -2686 229 19123475 2400 0

Node 6 Fxb 0 0 2400 75 0

Node 7 Fyb 0 -120 0 0 120

Node 8 Mzb -2400 0 8000000 2400 937

Node 9 Fxc -18 -23 286 -75 0

Node 10 Fyc -23 -29 -229 0 0

Mzc -286 229 1561738 0 938

Fxd

Fyd

Mzd

Fx

Fy

Mz

(APPLY BOUNDARY AND COMPATIBILITY CONDITIONS)

θza ub vb

Mza

=

0

=

19123475 2400 0

Fxb 0 2400 75 0

Fyb 0 0 0 120

Mzb 0 8000000 2400 937

Fxc 0 286 -75 0

Fyc 0 -229 0 0

Mzc 0 1561738 0 938

DISPLACEMENTS

θza ub vb

θza

=

0.00000 -0.00001 0.00000

[ Kff ]

{ Δ } = [ Kff ] 1 ̶� * { F }

Page 10: Exercise 041515

ub

=

-0.00001 0.07980 0.00008

vb 0.00000 0.00008 0.00832

θzb 0.00000 -0.00001 0.00000

uc -0.00001 0.06654 0.00007

vc 0.00000 -0.01031 0.00000

θzc 0.00000 -0.00001 0.00000

(APPLY BOUNDARY AND COMPATIBILITY CONDITIONS)

-0.0010 31.5989 -1.1729 -0.0154 31.2761

Fxa

=

-2685.7 -0.5 0.0 -2400.0 -18.3

Fya 228.5 0.0 -120.0 0.0 -22.8

Fxd 0.0 0.0 0.0 0.0 -0.5

Fyd 0.0 0.0 0.0 0.0 0.0

Mzd 0.0 0.0 0.0 0.0 2400.0

[ Ksf ]

Page 11: Exercise 041515

GLOBAL STIFFNESS MATRIX

θzb uc vc θzc ud vd θzd u v θz

-2400 -18 -23 -286

0 -23 -29 229

8000000 286 -229 1561738

2400 -75 0 0

937 0 0 938

21000000 0 -938 2500000

0 94 23 2686 0 0 2400

-938 23 149 -1166 0 -120 0

2500000 2686 -1166 24123475 -2400 0 8000000

0 0 -2400 0 0 -2400

0 -120 0 0 120 0

2400 0 8000000 -2400 0 16000000

(APPLY BOUNDARY AND COMPATIBILITY CONDITIONS)

θzb uc vc θzc FIXED-END FORCES

8000000 286 -229 1561738

+

0.0

2400 -75 0 0 0.0

937 0 0 938 120.0

21000000 0 -938 2500000 160000.0

0 94 23 2686 -537.6

-938 23 149 -1166 120.0

2500000 2686 -1166 24123475 -928000.0

DISPLACEMENTS

θzb uc vc θzc DISPLACEMENTS

0.00000 -0.00001 0.00000 0.00000 0

=

-0.0010 rad

[ Kff ]

{ Δ } = [ Kff ] 1 ̶� * { F }

Page 12: Exercise 041515

-0.00001 0.06654 -0.01031 -0.00001 0

=

31.5989 mm0.00000 0.00007 0.00000 0.00000 -120 -1.1729 mm0.00000 0.00000 0.00000 0.00000 -160000 -0.0154 rad0.00000 0.06659 -0.01031 -0.00001 537.6 31.2761 mm0.00000 -0.01031 0.00832 0.00000 -120 -5.4182 mm0.00000 -0.00001 0.00000 0.00000 928000 0.0364 rad

(APPLY BOUNDARY AND COMPATIBILITY CONDITIONS)

-5.4182 0.0364

-22.8 -285.7 -0.0010

=

-435.15582

-28.6 228.5 31.5989 -410.18731

0.0 -2400.0 -1.1729 -102.44418

-120.0 0.0 -0.0154 650.187313

0.0 8000000.0 31.2761 366501.495

-5.4182

0.0364

[ Ksf ]

Page 13: Exercise 041515

GLOBAL STIFFNESS MATRIX

FIXED-END FORCES

ua

+

va

θza

ub

vb

θzb

uc

vc

θzc

ud

vd

θzd

u

v

θz

Page 14: Exercise 041515

θza ub vb θzb uc vc θzc θza ub

19123475 2400 0 8000000 286 -229 1561738 24000000 24002400 75 0 2400 -75 0 0 2400 120

0 0 120 937 0 0 938 0 08000000 2400 937 21000000 0 -938 2500000 8000000 2400

286 -75 0 0 94 23 2686 1874 -120-229 0 0 -938 23 149 -1166 -1499 0

1561738 0 938 2500000 2686 -1166 24123475 4000000 0

0 0 0 0 0 0 0θza 0.00000 -0.00001 0.00000 0.00000 -0.00001 0.00000 0.00000ub -0.00001 0.07980 0.00008 -0.00001 0.06654 -0.01031 -0.00001vb 0.00000 0.00008 0.00832 0.00000 0.00007 0.00000 0.00000θzb 0.00000 -0.00001 0.00000 0.00000 0.00000 0.00000 0.00000uc -0.00001 0.06654 0.00007 0.00000 0.06659 -0.01031 -0.00001vc 0.00000 -0.01031 0.00000 0.00000 -0.01031 0.00832 0.00000θzc 0.00000 -0.00001 0.00000 0.00000 -0.00001 0.00000 0.00000

Mza -0.001048Fxb 31.59888Fyb -1.17292Mzb -0.015357Fxc 31.27613Fyc -5.418228Mzc 0.03643

Page 15: Exercise 041515

vb θzb uc vc θzc

2400 24000000 1874 -1499 40000000 2400 -120 0 0

121 2400 0 -1 24002400 24000000 0 -2400 4000000

0 0 168 58 4274-1 -2400 58 195 -3899

2400 4000000 4274 -3899 32000000

0 00 0

120 -120160000 -160000-537.6 537.6

120 -120-928000 928000

Page 16: Exercise 041515

θza ub θza ub vb θzb uc vc θzc

19123475 2400 -2686 0 0 -2400 -18 -23 -2862400 75 229 0 -120 0 -23 -29 229

0 0 -24000 -120 0

2400 0 8000000

Page 17: Exercise 041515

FIXED-END FORCES

Page 18: Exercise 041515

FIXED-END FORCES

Member bcDISPLACED NODE

Member cdDISPLACED NODE

Global Matrix for Fixed-End ForcesFxa 0Fya 6Mza 30000Fxb 0Fyb -32000Mzb 235.2Fxc 0Fyc -768000Mzc 608000Fxd 0Fyd 0Mzd 0Fxe 0Fye 0Mze 0

Page 19: Exercise 041515

Member bcDISPLACED NODE

q 30 120

L 8 160000200 120

50000000 -160000

Member cdDISPLACED NODE

P -600 -62.4

L 10 -192000

a 2 115.2

b 8 -768000

608000

Fy1, kNMz1, kN∙mm

E, GPa Fy2, kN

I, mm4 Mz2, kN∙mm

Fy1, kNMz1, kN∙mmFy2, kNMz2, kN∙mm