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 Public Deposited

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

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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  • description.provenance : Made available in DSpace on 2006-04-11T15:00:41Z (GMT). No. of bitstreams: 1 FPL_1583ocr.pdf: 14219113 bytes, checksum: 432c449341a01784acb2d9652849f631 (MD5) Previous issue date: 1955-08
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