- Wrapped Thick Composite Cylinder under Pressure and Thermal Loading
Determine the circumferential stress at different radial locations of a wrapped thick cylinder subjected to the following loads:
- Composite Laminate under Three-Point Bending
Subject a composite laminate with a layup [0/90/0/90/0/90/0] to three point bending with support span = 30 mm by applying a uniform load of P = 10 N/mm at the center. Find the longitudinal stress SX and displacement UY at point B and transverse shear stress TXY at point C.
- Sandwich Composite Shell under Pressure
Subject a simply-supported sandwich shell (two outer facing sheets and an inner core) to a uniform normal pressure of 100 psi. Determine the central transverse displacement (top surface), SX and SY stresses at center of the top sheet, and TXY stress at the quarter point of the top sheet.