Journal of Mechanics of Materials and Structures vol. 5 (2010 ... - MSP
Journal of Mechanics of Materials and Structures vol. 5 (2010 ... - MSP
Journal of Mechanics of Materials and Structures vol. 5 (2010 ... - MSP
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
808 YING LI AND CHANG-JUN CHENG<br />
3. The Hamilton principle <strong>and</strong> mathematical model <strong>of</strong> thermoelastic beams with voids<br />
In order to present the nonlinear mathematical model <strong>of</strong> the problem, we first derive a generalized Hamilton<br />
principle for thermoelastic beams with voids under geometric nonlinearity.<br />
Let<br />
� �<br />
��<br />
Mϕ = ϕ(xi, t)x2x3 dA <strong>and</strong> Mθ = θ(xi, t)x2x3 dA (6)<br />
A<br />
A<br />
be the moments caused by the change <strong>of</strong> the <strong>vol</strong>ume fraction ϕ(xi, t) <strong>and</strong> temperature θ(xi, t), respectively.<br />
Set<br />
� �<br />
qϕ = αv x2x3(ϕ,22 + ϕ,33) dA<br />
A<br />
�� b/2<br />
= αv<br />
−b/2<br />
qθ = K<br />
� �<br />
�<br />
(x3ϕ,3)| h/2<br />
�<br />
� h/2 �<br />
−h/2 − ϕ|h/2<br />
−h/2<br />
x2 dx2 + (x2ϕ,2)|<br />
−h/2<br />
b/2<br />
�<br />
�<br />
−b/2 − ϕ|b/2<br />
−b/2<br />
x3 dx3 ,<br />
x2x3(θ,22 + θ,33) dA<br />
T0 A<br />
�� b/2<br />
= K<br />
T0<br />
−b/2<br />
�<br />
(x3θ,3)| h/2<br />
�<br />
� h/2 �<br />
−h/2 − θ|h/2<br />
−h/2<br />
x2 dx2 + (x2θ,2)|<br />
−h/2<br />
b/2<br />
�<br />
�<br />
−b/2 − θ|b/2<br />
−b/2<br />
x3 dx3 .<br />
According to [Cowin <strong>and</strong> Nunziato 1983], on the surfaces <strong>of</strong> the beam, ϕ(xi, t) needs to satisfy the<br />
conditions ϕ,2|x2=±b/2 = 0 <strong>and</strong> ϕ,3|x3=±h/2 = 0, so the expression for qϕ simplifies to<br />
� � b/2<br />
� h/2<br />
qϕ = −αv<br />
(ϕ| b/2<br />
−b/2 )x3<br />
�<br />
dx3<br />
(8)<br />
(ϕ|<br />
−b/2<br />
h/2<br />
−h/2 )x2 dx2 +<br />
−h/2<br />
The thermal boundary conditions <strong>of</strong> the beam may be given as<br />
K θ,2|x2=b/2 = ¯h(T∞ − θb/2), K θ,2|x2=−b/2 = −¯h(T∞ − θ−b/2),<br />
K θ,3|x3=h/2 = ¯h(T∞ − θh/2), K θ,3|x3=−h/2 = −¯h(T∞ − θ−h/2),<br />
where ¯h is the heat transfer coefficient, θb/2, θ−b/2, θh/2, <strong>and</strong> θ−h/2 denote the temperatures on the<br />
surfaces x2 = ±b/2 <strong>and</strong> x3 = ±h/2, <strong>and</strong> T∞ is the temperature <strong>of</strong> surrounding medium. If we assume<br />
that T∞ = 0, the absolute temperature is equal to the reference temperature. The second expression <strong>of</strong><br />
(7) then simplifies to<br />
� � b/2<br />
h ¯h/2 + K<br />
qθ = −<br />
(θ| h/2<br />
−h/2 )x2 dx2 + b¯h/2<br />
� h/2 + K<br />
(θ| b/2<br />
−b/2 )x3<br />
�<br />
dx3 . (10)<br />
T0<br />
−b/2<br />
To evaluate (8) <strong>and</strong> (10), we express the change <strong>of</strong> the <strong>vol</strong>ume fraction <strong>and</strong> temperature as the series<br />
ϕ(xi, t) =<br />
∞�<br />
Substituting (11) into (6) yields<br />
m=0 n=0<br />
T0<br />
∞�<br />
ϕmn(x1, t)x m 2 xn 3 ,θ(xi, t) =<br />
∞�<br />
−h/2<br />
m=0 n=0<br />
∞�<br />
ϑmn(x1, t)x m 2 xn 3<br />
(7)<br />
(9)<br />
(11)<br />
Mϕ = Aϕ11(x1, t) + o(b 3 h 3 ) , Mθ = Aϑ11(x1, t) + o(b 3 h 3 ), (12)