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Creator:: Forest Products Laboratory (U.S.) and Haft, Everett Eugene
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: used. Prebuckling Stresses Before buckling occurs the cylinder is in a state of uniform compression

Creator:: Forest Products Laboratory (U.S.), Kommers, William J., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed 1962.
Resource Type:: Technical Report
Full Text:: Report No . 1583 presents the- mathematical analysis for the buckling of sand - wich materials under

Creator:: Forest Products Laboratory (U.S.) and March, H. W.
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 August 1955.
Resource Type:: Technical Report
Full Text:: buckling loads of flat sandwich panels under unifor m compression along two opposite edges and subject to

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Kommers, William J.
Abstract:: Information reviewed and reaffirmed 1958. Original report issued June 1952.
Resource Type:: Technical Report
Full Text:: these panels so that they will not fail elastically by buckling when subjected to such loads, the values

Creator:: Forest Products Laboratory (U.S.) and Raville, Milton E.
Abstract:: Information reviewed and reaffirmed in 1960.
Resource Type:: Technical Report
Full Text:: LABORATORY ‘<, Nitictiso, 5, Wiscorv-siii In Cooperation_with the University of Wisconsin, BUCKLING OF

Creator:: Forest Products Laboratory (U.S.) and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce
Resource Type:: Technical Report
Full Text:: formulas for the buckling loads of rectangular sandwich panels subjected to edgewise compression is given

Creator:: Forest Products Laboratory (U.S.), March, H. W., and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce. Revised December 1957. Original report published June 1952.
Resource Type:: Technical Report
Full Text:: Laboratory Report No. 1312. (7) 1943. Buckling of Long, Thin Plywood Cylinders in Axial Compression

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed 1962. Report originally issued in 1943.
Resource Type:: Technical Report
Full Text:: ison, Wiscons in S3 lO5 Supplernent to BUCKLING OI'FLAT PLYWOOD PLATES IN COMPRESSION' SHEAR, OR

Creator:: March, H. W. and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed 1958. Original report issued September 1952.
Resource Type:: Technical Report
Full Text:: the compressive buckling of a sandwich panel with simply supported edges and with the facings treated

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed March 1956. Original report issued December 1946.
Resource Type:: Technical Report
Full Text:: sandwich constructio n under axially compressive loads . The axial buckling strength of a well-made, long

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