Fatigue of sandwich constructions for aircraft : Aluminum facing and expanded-aluminum-honeycomb core sandwich material tested in shear Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/sj1395816

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on aircraft design criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed 1958. Original report issued July 1952.

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  • description.provenance : Made available in DSpace on 2006-04-17T18:40:49Z (GMT). No. of bitstreams: 1 FPL_1559-Kocr.pdf: 5396952 bytes, checksum: 4503861ba49ee88ab2ad2b9c88681520 (MD5) Previous issue date: 1958
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