Forest Products Laboratory; [Research report] R-564-R1691 (with omissions). 1525-B. Buckling loads of flat sandwich panels in compression: Buckling of flat sandwich panels with loaded edges simply supported and remaining edges clamped (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 simply supported and remaining edges clamped (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-B. Buckling loads of flat sandwich panels in compression: Buckling of flat sandwich panels with loaded edges simply supported and remaining edges clamped (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.]