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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
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