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

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dc.date 2006-04-11T16:35:46Z
dc.date 2006-04-11T16:35:46Z
dc.date 1962
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/1957/1624
dc.identifier.uri http://koha.mediu.edu.my:8181/xmlui/handle/1957/1624
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. Information reviewed and reaffirmed 1956 and 1962. Original report issued October 1948.
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-E
dc.title Fatigue of sandwich constructions for aircraft : Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear
dc.type Book


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