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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: 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
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
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