A general framework for interpreting time finite element formulations M. BorriC. Bottasso Originals Pages: 133 - 142
Some computational tools for the analysis of through cracks in stiffened fuselage shells C. C. RankinF. A. BroganE. Riks Originals Pages: 143 - 156
Structural topology and shape optimization for a frequency response problem Z. -D. MaN. KikuchiI. Hagiwara Originals Pages: 157 - 174
A nonlinear composite shell element with continuous interlaminar shear stresses F. GruttmannW. WagnerP. Wriggers Originals Pages: 175 - 188
Fatigue growth of multiple-cracks near a row of fastener-holes in a fuselage lap-joint J. H. ParkS. N. Atluri Originals Pages: 189 - 203
A general formulation for the nonlinear dynamics and control of orbiting flexible structures V. J. ModiA. C. NgF. Karray Originals Pages: 204 - 230