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An experimental nondestructive method for determining the buckling load of a column with arbitrary end conditions

Creator:: Balch, Robert Lyle
Resource Type:: Masters Thesis
Full Text:: buckling load of a column with arbitrary end conditions :4 AN EXPRINENTAL NONDESTFUCTIVE FTHOD FOR

Supplement to compression, tension, and shear tests on yellow-poplar plywood panels of sizes that do not buckle with tests made at various angles to the face grain : shear tests

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, McKinnon, P. F., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed, 1962. Original report published 1945.
Resource Type:: Technical Report

Buckling of simply supported rectangular sandwich panels subjected to edgewise bending

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:: BUCKLING OF SIMPLY SUPPORTED RECTANGULAR SANDWICH PANELS SUBJECTED TO EDGEWISE BENDING! By W. E. JAHNKE

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: Information reviewed and reaffirmed in 1962.
Resource Type:: Technical Report
Full Text:: Elements for Case a = 2, E = 00 103c X. FIGURES 121 ELASTIC BUCKLING OF A SIMPLY SUPPORTED

Compressive buckling curves for sandwich panels with isotropic facings and isotropic or orthotropic cores

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 Sandwich Construction of the Departments of the Air Force, Navy, and Commerce. Revised January 1958.
Resource Type:: Technical Report
Full Text:: LABORATORY MADISON 5. WISCONSIN COMPRESSIVE BUCKLING CURVES FOR FLAT SANDWICH PANELS 1 WITH ISOTROPIC

Effect of axial stiffeners on the buckling properties of thin curved plywood plates in axial compression

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:: STIFFENERS ON THE BUCKLING PROPERTIES OF THIN CURVED PLYWOOD PLATES IN AXIAL COMPRESSION1 By FRED WERREN

A single stiffener perpendicular to stress

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

Stresses within a rectangular, flat sandwich panel subjected to a uniformly distributed normal load and edgewise, direct, and shear loads

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Kommers, William J., 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.
Resource Type:: Technical Report
Full Text:: blocks at their outer edges, to keep the specimens from buckling as a whole. Three dial gages were

Design curves for the buckling of sandwich cylinders of finite length under uniform external lateral pressure

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Zahn, John J.
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:: FOR THE !BUCKLING Of SANDWICH CYLINDERS Of FINITE LENGTH UNDER UNIFORM EXTERNAL LATERAL PRESSURE

Buckling of sandwich cylinders in torsion

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:: CONSTRUCTION of the [Departments of the AIR FORCE, NAVY, ANC) COMMERCE BUCKLING OF SANDWICH CYLINDERS IN

ScholarsArchive@OSU

An experimental nondestructive method for determining the buckling load of a column with arbitrary end conditions

Supplement to compression, tension, and shear tests on yellow-poplar plywood panels of sizes that do not buckle with tests made at various angles to the face grain : shear tests

Buckling of simply supported rectangular sandwich panels subjected to edgewise bending

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression

Compressive buckling curves for sandwich panels with isotropic facings and isotropic or orthotropic cores

Effect of axial stiffeners on the buckling properties of thin curved plywood plates in axial compression

A single stiffener perpendicular to stress

Stresses within a rectangular, flat sandwich panel subjected to a uniformly distributed normal load and edgewise, direct, and shear loads

Design curves for the buckling of sandwich cylinders of finite length under uniform external lateral pressure

Buckling of sandwich cylinders in torsion

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