Forest Products Laboratory; [Research report] R-564-R1691 (with omissions). 1525-C. Buckling loads of flat sandwich panels in compression: Buckling of flat sandwich panels with loaded edges clamped and remaining edges simply supported (cores of end-grain balsa or cellular cellulose acetate and faces of aluminum or glass cloth laminate); [by K. H. Boller].
Publication Title:
Buckling loads of flat sandwich panels in compression: Buckling of flat sandwich panels with loaded edges clamped and remaining edges simply supported (cores of end-grain balsa or cellular cellulose acetate and faces of aluminum or glass cloth laminate); [by K. H. Boller].
Display Title:
Forest Products Laboratory; [Research report] R-564-R1691 (with omissions). 1525-C. Buckling loads of flat sandwich panels in compression: Buckling of flat sandwich panels with loaded edges clamped and remaining edges simply supported (cores of end-grain balsa or cellular cellulose acetate and faces of aluminum or glass cloth laminate); [by K. H. Boller].
[This report is one of a series issued in cooperation with Army-Navy-Civil Committee on Aircraft Design Criteria under supervision of Aeronautical Board.] and [Processed.]