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Fatigue of sandwich constructions for aircraft : Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear Public Deposited
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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 1956 and 1962. Original report issued October 1948.
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