Analysis of Orthotropic, Laminated Shells with Shear Deformations.
ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL ALA GROUND EQUIPMENT/MATERIALS DIRECTORATE
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A curved finite element is developed for the analysis of a laminated, axisymmetric shell of revolution with transverse shear deformation. The element stiffness relations are obtained from the principle of minimum potential energy. The shell displacements represent four degrees of freedom at a node, two translation, two rotation. Author
- Numerical Mathematics
- Structural Engineering and Building Technology
- Guided Missiles