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Buckling loads of flat sandwich panels in compression : The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate) Public Deposited
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This report is one of a series issued in cooperation withe the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed Janary 1954 and 1960.
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