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Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated March 1948.
Resource Type:: Technical Report
Full Text:: with the University of Wisconsin BUCKLING LOADS OF FLAT SANDWICH PANELS IN COMPRESSION- The

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: COMPRESSION- Buckling of Flat Sandwich Panels With All Edges Clamped-- (Cores of End-grain Balsa or

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: COMPRESSION- Buckling of Flat Sandwich Panels with Loaded Edges Clamped and the Remaining Edges Simply

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: OF FLAT SANDWICH PANELS IN COMPRESSION— Buckling of Flat Sandwich Panels with Loaded Edges Simply

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: 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 January 1954 and 1960.
Resource Type:: Technical Report
Full Text:: SANDWICH PANELS IN COMPRESSION-1 The Buckling of Flat Sandwich Panels with Edges Simply Supported_ (End

Creator:: March, H. W., Smith, C. B., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956 and 1962. Original report published in 1945.
Resource Type:: Technical Report
Full Text:: curves for determining the buckling loads in compression of flat sandwich panels of various constructions

Creator:: Forest Products Laboratory (U.S.), Werren, Fred, and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: 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. Reviewed and reaffirmed March 1956. Original report issued March 1948.
Resource Type:: Technical Report
Full Text:: axial stiffener to a curved plywood plate in compression does not increase the buckling stress of the

Creator:: Forest Products Laboratory (U.S.), Heebink, T. B. (Thomas Bruce), 1914-, March, H. W., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed March 1956. Original report published in 1946.
Resource Type:: Technical Report
Full Text:: BUCKLING OF STI.P.PENED, FLAT PLYWOOD PLATES IN COMPRESSION-- A

Creator:: Heebink, T. B. (Thomas Bruce), 1914-, Norris, Charles, B. (Charles Brazer), 1894-, and Forest Products Laboratory (U.S.)
Abstract:: 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 1956 and 1962. Original report issued 1946.
Resource Type:: Technical Report
Full Text:: Supplement to BUCKLING Of STIFFENED, FIAT, PLYWOOD IPLATIES IN

Creator:: Forest Products Laboratory (U.S.), Heebink, Bruce G., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed August 1961. This report was originally issued in February 1950.
Resource Type:: Technical Report
Full Text:: The critical buckling stress of a curved plywood panel subjected to axial compression can be increased

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