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Determination of desirable lengths of Z- and channel-section columns for local-instability tests

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded R303-T Aluminum Alloy

Column and plate compressive strengths of aircraft structural materials: 17S-T aluminum-alloy sheet

Column and plate compressive strengths of aircraft structural materials: extruded 75S-T aluminum alloy

Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-Alloy Sheet

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Column and plate compressive strengths of aircraft structural materials: extruded 24S-T aluminum alloy

Effect of brake forming on the strength of 24S-T aluminum-alloy sheet

Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 14S-T Aluminum Alloy

Determination of plate compressive strengths

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 0-1HTA Magnesium Alloy

Determination of plate compressive strengths at elevated temperatures

Determination of plate compressive strengths at elevated temperatures

Structural efficiencies of various aluminum, titanium, and steel alloys at elevated temperatures

Tensile properties of some sheet materials under rapid-heating conditions

Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load

Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions

Generalized master curves for creep and rupture


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