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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

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https://ir.library.oregonstate.edu/concern/defaults/5q47rs72s

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  • 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.
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  • Scanned at 600 DPI using a Canon DR-9080C in TIF format. PDF generated through Capture Perfect using OmniPage 14 Pro for textual OCR.
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