MSC

Structural Mechanics Calculators

Synopsis

The calculator computes the effective laminate thermal expansion coefficients. Six coefficients are returned. The alpha terms give the thermal expansion strain at the laminate midplane. The gamma terms are the thermal curvature coefficients. Nonsymmetric laminates will curve due to a change in temperature.


Input

Enter the layer material properties as a list {Ex, Ey, Gxy, nuxy}:




Enter the layer thermal expansion coefficients {alpha x, alpha y}



Enter a stacking sequence {theta1, theta2, ...}: Help on advanced stack entry


Check to tabulate expanded stacking sequence


Result



Usage Notes

Page History Notes