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Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear

Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear

URI: http://koha.mediu.edu.my:8181/xmlui/handle/1957/1625
Date: 2013-10-16

Description:

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.

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