Stresses within a rectangular, flat sandwich panel subjected to a uniformly distributed normal load and edgewise, direct, and shear loads Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/w3763b51q

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.

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  • description.provenance : Made available in DSpace on 2006-06-12T22:12:33Z (GMT). No. of bitstreams: 1 FPL_1838ocr.pdf: 2982515 bytes, checksum: 3e298a7b33db48cffb572a83d2d5d36f (MD5) Previous issue date: 1953-01
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