Index Catalog // ScholarsArchive@OSU

Plastic flow throughout volume of thin adhesive bonds

Creator:: Forest Products Laboratory (U.S.) and Norris, Charles, B. (Charles Brazer), 1894-
Resource Type:: Technical Report

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

Compressive buckling curves for simply supported sandwich panels with glass-fabric-laminate facings and honeycomb 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 Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce
Resource Type:: Technical Report

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

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

Effect of unbonded joints in an aluminum honeycomb-core material for sandwich constructions

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 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 May 1952.
Resource Type:: Technical Report

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

Short-column compressive strength of sandwich constructions as affected by the size of the cells of honeycomb-core materials

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 ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report

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

Creep tests of sandwich constructions subjected to shear at normal temperatures

Creator:: Forest Products Laboratory (U.S.), Voss, Arnold W., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: In cooperation with the U.S. Air Force. Information reviewed and reaffirmed May 1954. This report was originally published in May 1949.
Resource Type:: Technical Report

Directional properties of glass-fabric-base plastic laminate panels of sizes that do not buckle

Creator:: Warren, Fred, Norris, Charles, B. (Charles Brazer), 1894-, and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956. Original report published April 1949.
Resource Type:: Technical Report

Critical buckling strength of stiffened flat plywood plates in compression and shear-closely spaced stiffeners

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, Kommers, William J., and McKinnon, P. F.
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 February 1948.
Resource Type:: Technical Report

Longitudinally stiffened thin-walled plywood cylinders in axial compression

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

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

The effect of a stiffener on the maximum load of flat plywood plates in edgewise compression, with the face grain at 0 degrees and 90 degrees to the load : A single stiffener parallel to the direction of loading : Load edges clamped, others simply supported

Creator:: Ringelstetter, L. A., Norris, Charles, B. (Charles Brazer), 1894-, and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report

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

A single stiffener parallel to stress face grain of plywood at 45 degrees to its edges

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Ringelstetter, L. A.
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 March 1956. Original report issued October 1948.
Resource Type:: Technical Report

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

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

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and McKinnon, P. F.
Abstract:: Information reviewed and reaffirmed, 1962. Original report published in 1946. 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

Supplement to the flexural rigidity of a rectangular strip of sandwich construction

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Ericksen, Wilhelm S., Kommers, William J., and Forest Products Laboratory (U.S.)
Abstract:: Supplementary mathematical analysis and comparison with the results of tests. 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

ScholarsArchive@OSU

Plastic flow throughout volume of thin adhesive bonds

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

Compressive buckling curves for simply supported sandwich panels with glass-fabric-laminate facings and honeycomb cores

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

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

Effect of unbonded joints in an aluminum honeycomb-core material for sandwich constructions

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

Short-column compressive strength of sandwich constructions as affected by the size of the cells of honeycomb-core materials

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

Creep tests of sandwich constructions subjected to shear at normal temperatures

Directional properties of glass-fabric-base plastic laminate panels of sizes that do not buckle

Critical buckling strength of stiffened flat plywood plates in compression and shear-closely spaced stiffeners

Longitudinally stiffened thin-walled plywood cylinders in axial compression

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

The effect of a stiffener on the maximum load of flat plywood plates in edgewise compression, with the face grain at 0 degrees and 90 degrees to the load : A single stiffener parallel to the direction of loading : Load edges clamped, others simply supported

A single stiffener perpendicular to stress

A single stiffener parallel to stress face grain of plywood at 45 degrees to its edges

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

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

Supplement to the flexural rigidity of a rectangular strip of sandwich construction

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