Novel composites for wing and fuselage applications

Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784

By Dave Sharp

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Publish Date

1997

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Mechanical properties, Panels, Buckling, Tensile stress, Load carrying capacity, Shear strain, Tensile strength, Shear strength, Composite structures, Shear stress