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Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: Original report issued October 1944.
Resource Type:: Technical Report
Full Text:: the theory for long cylinders in compression . ± This theory showe d that the buckling constant k

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward 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 1960.
Resource Type:: Technical Report
Full Text:: cylinders in compression. Plates of smaller widths and lengths exhibit higher buckling stresses. Scope of

Creator:: Forest Products Laboratory (U.S.), Jahnke, W. E., and Kuenzi, Edward W.
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:: rates for the tension side of the beam. The buckling load occurred at 15,500 pounds when the compression

Creator:: Forest Products Laboratory (U.S.), March, H. W., Norris, Charles, B. (Charles Brazer), 1894-, Smith, C. B., and Kuenzi, Edward W.
Abstract:: Information reviewed and reaffirmed August 1960. Original report dated June 1945.
Resource Type:: Technical Report
Full Text:: in footnote 4 . Also the paper, "The Buckling Of -Thin-Cylindrical Shells under Axial Compression

Creator:: Forest Products Laboratory (U.S.), March, H. W., and Kuenzi, Edward W.
Abstract:: Originally prepared and distributed in June 1953. Revised December 1957. Information reviewed and reaffirmed in 1965.
Resource Type:: Technical Report
Full Text:: . Buckling of Sandwich Cylinders in Axial Compression. Forest Products Laboratory Report No. 1830. MARCH, H

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.) 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

Creator:: Forest Products Laboratory (U.S.), Kuenzi, Edward W., 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. Information reviewed and reaffirmed March 1956. Original report issued April 1948.
Resource Type:: Technical Report
Full Text:: prepared for testing in compression by gluing together six 1- by 4-inch pieces. The pieces were not glued

Creator:: Youngquist, W. G., Kuenzi, Edward 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 1960. Original report issued March 1955.
Resource Type:: Technical Report
Full Text:: test method used in testing the panels is illustrated in figure 3. The 20-inch-diameter panels were

Creator:: Kuenzi, Edward W., Ericksen, Wilhelm S., Zahn, John J., and Forest Products Laboratory (U.S.)
Abstract:: Revised May 1962. Original report dated May 1947.
Resource Type:: Technical Report
Full Text:: buckling loads than would apparatus of the compression type. The compression arrangement was unsatisfactory

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