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Formulas for columns with side loads and eccentricity

Creator:: Wood, Lyman Wentsch, 1899- and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: receive both compression and flexural stresses under eccentric axial load, but it is not necessary to

Stresses induced in a sandwich panel by load applied at an insert

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:: STRESSES INDIUM IN A SANUIVICE PANEL ITY LOAD APPLIED AT AN INSERT

Wrinkling of the facings of sandwich construction subjected to edgewise compression : sandwich constructions having honeycomb cores

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, Boller, Kenneth H., and Voss, Arnold W.
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.
Resource Type:: Technical Report
Full Text:: perfectly flat, so that deflections occur at small loads and increase more and more rapidly as the load

Simply supported sandwich beam : a nonlinear theory

Creator:: Forest Products Laboratory (U.S.) and Zahn, John J.
Resource Type:: Technical Report
Full Text:: load and the results are shown in a series of curves. Numerical work was performed with the aid of

Theoretical design of a nailed or bolted joint under lateral load

Creator:: Kuenzi, Edward W. and Forest Products Laboratory (U.S.)
Abstract:: Originally issued in September 1953. Revised March 1955. Information reviewed and reaffirmed 1960.
Resource Type:: Technical Report
Full Text:: THEORETICAL DESIGN OF A NAILED OR HATED JOINT UNDER LATERAL LOAD

Supplement to deflection and stresses in a uniformly loaded, simply supported, rectangular sandwich plate : experimental verification of theory

Creator:: Lewis, Wayne C., 1914- and Forest Products Laboratory (U.S.)
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. Information reviewed and reaffirmed 1962. Original report issued December 1956.
Resource Type:: Technical Report
Full Text:: veri- fication of the mathematical derivations presented in Report 1847. Panels 20 by 20 and 20 by 30

Deflection and stresses in a uniformly loaded, simply supported, rectangular sandwich plate

Creator:: Forest Products Laboratory (U.S.) and Raville, Milton E.
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. Information reviewed and reaffirmed September 1962. Original report dated December 1955.
Resource Type:: Technical Report
Full Text:: . 1847 orthotropic core. The core is considered to have such a small load- carrying capacity in the

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:: A UNIFORMLY DISTRIEUTED NORMAL LOAD AND EDGEWISE, DIRECT, AND WEAR LOADS January 1953 This Report

Transfer of longitudinal load from one facing of a sandwich panel to the other by means of shear in the core

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Boller, Kenneth H.
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. Information reviewed and reaffirmed 1960. Original report issued April 1955.
Resource Type:: Technical Report
Full Text:: LOAD FROM ONE FACING OF A SANDWICH PANEL TO THE OTHER BY MEANS OF SHEAR IN THE CORE! By CHARLES B

Critical loads of a rectangular, flat sandwich panel subjected to two direct loads combined with a shear load

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:: TWO DIRECT LOADS COMBINED WITH A SHEAR LOAD No. 1833 June 1952 INFORMATION REVIEWED AND REAFFIRMED

ScholarsArchive@OSU

Formulas for columns with side loads and eccentricity

Stresses induced in a sandwich panel by load applied at an insert

Wrinkling of the facings of sandwich construction subjected to edgewise compression : sandwich constructions having honeycomb cores

Simply supported sandwich beam : a nonlinear theory

Theoretical design of a nailed or bolted joint under lateral load

Supplement to deflection and stresses in a uniformly loaded, simply supported, rectangular sandwich plate : experimental verification of theory

Deflection and stresses in a uniformly loaded, simply supported, rectangular sandwich plate

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

Transfer of longitudinal load from one facing of a sandwich panel to the other by means of shear in the core

Critical loads of a rectangular, flat sandwich panel subjected to two direct loads combined with a shear load

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