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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


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