Static and fatigue strengths of high-strength aluminum-alloy bolted joints
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ALUMINUM ALLOYS - STRENGTH, EFFECT OF NOTCHES↗
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Plastic buckling of extruded composite sections in compression
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PLATES - BUCKLING↗
Fatigue strengths of aircraft materials : axial-load fatigue tests on notched sheet specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with stress-concentration factor of 5.0
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ALUMINUM ALLOYS - ALCOA 75ST6 - FATIGUE↗
Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels Having Small, Thin, Widely Spaced, Longitudinal Extruded Z-Section Stiffeners
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ALUMINUM ALLOYS - EXTRUSION↗
Effect of variation in rivet diameter and pitch on the average stress at maximum load for 24S-T3 and 75S-T6 aluminum-alloy, flat, Z-stiffened panels that fail by local instability
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ALUMINUM ALLOYS - ALCOA 75ST6↗
Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels with Longitudinal Extruded Z-Section Stiffeners
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ALUMINUM ALLOYS - ALCOA 75ST6 - STRENGTH, COMPRESS↗
Comparison of the Structural Efficiency of Panels Having Straight-web and Curved-web Y-section Stiffeners
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STRESSED SKIN - PLATES↗
Effect of open circular holes on tensile strength and elongation of sheet specimens of some aluminum alloys
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ALUMINUM ALLOYS - ALCOA 24ST86↗
Determination of Plate Compressive Strengths at Elevated Temperatures
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PLATES, FLAT - COMPRESSION↗
Elevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy
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ALUMINUM ALLOYS - TEMPERATURES↗
Stress-strain and elongation graphs for aluminum-alloy 75S-T6 sheet
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DIAGRAMS, STRESS-STRAIN↗
The Effect of Nonuniform Temperature Distributions on the Stresses and Distortions of Stiffened-Shell Structures
The structural effects of nonuniform temperature distributions, such as those produced by aerodynamic heating or thermal ice-prevention systems, are discussed and found to be of two types: The introduction of thermal stresses and distortions as a result of restrained thermal expansion and a change in the stresses and distortions produced by the applied loads as a result of the variation of elastic properties of materials with temperature. These effects are illustrated by sample analyses of the stress and distortion distributions of simple box beams and by calculation of the stresses on a typical wing section.
ALUMINUM ALLOYS - ALCOA 75ST6 - ELASTICITY↗
Fatigue Strengths of Aircraft Materials : Axial Load Fatigue Tests on Unnotched Sheet Specimens of 24S-T3 and 75S-T6 Aluminum Alloys and of SAE 4130 Steel
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ALUMINUM ALLOYS - ALCOA 24ST3 - FATIGUE↗
A structural-efficiency evaluation of titanium at normal and elevated temperatures
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PLATES, STRUCTURAL↗