AIAA Journal

AIAA Journal

4.11 - 1251 ratings - Source

[11] Johnson, E. H., MSC/NASTRAN Design Sensitivity and Optimization, Usera#39;s Guide. ... of classical laminated-plate theory K = buckling coefficient Nh = stress resultant for maximum axial compression under bending Nx = axial compression anbsp;...

Title:AIAA Journal
Author:American Institute of Aeronautics and Astronautics
Publisher: - 2008


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