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

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dc.date 2006-04-11T16:47:32Z
dc.date 2006-04-11T16:47:32Z
dc.date 1948-12
dc.date.accessioned 2013-10-16T07:32:01Z
dc.date.available 2013-10-16T07:32:01Z
dc.date.issued 2013-10-16
dc.identifier http://hdl.handle.net/1957/1625
dc.identifier.uri http://koha.mediu.edu.my:8181/xmlui/handle/1957/1625
dc.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.
dc.language en_US
dc.publisher Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory
dc.relation Report (Forest Products Laboratory (U.S.))
dc.relation no. 1559-F
dc.title Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear
dc.type Book


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