Effects of shear deformation in the core of a flat rectangular sandwich panel : 1. Buckling under compressive end load. 2. Deflection under uniform transverse load
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Effects of shear deformation in the core of a flat rectangular sandwich panel : 1. Buckling under compressive end load. 2. Deflection under uniform transverse load
This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the Aeronautical Board.
Information reviewed and reaffirmed August 1955.