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Effects of shear deformation in the core of a flat rectangular sandwich panel : 1. Buckling under compressive end load. 2. Deflection under uniform transverse load

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dc.date 2006-04-11T15:00:41Z
dc.date 2006-04-11T15:00:41Z
dc.date 1955-08
dc.date.accessioned 2013-10-16T07:32:13Z
dc.date.available 2013-10-16T07:32:13Z
dc.date.issued 2013-10-16
dc.identifier http://hdl.handle.net/1957/1616
dc.identifier.uri http://koha.mediu.edu.my:8181/xmlui/handle/1957/1616
dc.description This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed August 1955.
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.1583
dc.title Effects of shear deformation in the core of a flat rectangular sandwich panel : 1. Buckling under compressive end load. 2. Deflection under uniform transverse load
dc.type Book


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