**OS-V: 0500 Laminated Strip**

Test No. R0031/1 OptiStruct examines the bending stress at E, Interlaminar shear stress at D and the z-deflection at E for linear static analysis.**OS-V: 0510 Wrapped Thick Cylinder**

Test No: R0031/2 OptiStruct examines the hoop stress in the inner and outer cylinder at different radius for linear static analysis.**OS-V: 0520 Sandwich Shell**

Test No: R0031/3 OptiStruct examines the z deflection at C, Normal XX stress at C, Normal YY stress at C and Shear stress at E for linear static analysis.**OS-V: 0530 Composite Shell Bending**

This problem discusses the composite shells two- or three-layer plate subjected to a sinusoidal distributed load, as described by Pagano (1969).**OS-V: 0531 Laminated Shell Strength Analysis Mechanical Load 1**

This problem analyzes the strength of laminated composite shells when subjected to a uniform longitudinal load per unit length.**OS-V: 0532 Laminated Shell Strength Analysis Mechanical Load 2**

This problem analyzes the strength of laminated composite shells when subjected to a more general combination of membrane and bending load.**OS-V: 0533 Laminated Shell Strength Analysis Mechanical Load 3**

This problem demonstrates when the loads applied in OS-V: 0532 are factored by 1.1491, a Hill failure index (FI) and a reserve factor (RF) of unity for ply 1 are obtained.**OS-V: 0534 Laminated Shell Strength Analysis Thermal Load 1**

This problem analyzes the strength of laminated composite shells when subjected to a uniform constant temperature.