Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

(nextflipdebug5) #1
6.8 Finite Element Method for Continuum Structures 197

Thetotalpotentialenergyofthebeamhasastationaryvaluewithrespecttothenodaldisplacements
{δe}T;hence,fromEq.(6.71),


∂(U+V)
∂{δe}T

=


vol

[A−^1 ]T[C]T[D][C][A−^1 ]{δe}d(vol)−{Fe}= 0 (6.72)

fromwhich


{Fe}=




vol

[C]T[A−^1 ]T[D][C][A−^1 ]d(vol)


⎦{δe} (6.73)

orwriting[C][A−^1 ]as[B]weobtain


{Fe}=




vol

[B]T[D][B]d(vol)


⎦{δe} (6.74)

fromwhichtheelementstiffnessmatrixisclearly


[Ke]=




vol

[B]T[D][B]d(vol)


⎦ (6.75)

FromEqs.(6.62)and(6.64),wehave


[B]=[C][A−^1 ]=[0026x]






1000

0100

− 3 /L^2 − 2 /L 3 /L^2 − 1 /L

2 /L^31 /L^2 − 2 /L^31 /L^2






or


[B]T=

⎡ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎢ ⎣


6

L^2

+

12 x
L^3


4

L

+

6 x
L^2
6
L^2


12 x
L^3


2

L

+

6 x
L^2

⎤ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎥ ⎦

(6.76)
Free download pdf