Test No: R0031/3OptiStruct 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.
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: 0500 Laminated Strip Test No. R0031/1OptiStruct 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: R0031/2OptiStruct examines the hoop stress in the inner and outer cylinder at different radius for linear static analysis.
OS-V: 0520 Sandwich Shell Test No: R0031/3OptiStruct 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 about the composite shells two- or three-layer plate subjected to a sinusoidal distributed load, as described by Pagano (1969).