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Guides for preventing buckling in axial fatigue tests of thin sheet-metal specimens

Axial Fatigue of 10 Airplane Wing-Beam Specimens by the Resonance Method

Axial Fatigue Tests at Zero Mean Stress of 24S-T Aluminum-Alloy Sheet With and Without a Circular Hole

Axial Fatigue Test at Two Stress Amplitudes of 0.032-Inch 24S-T Sheet Specimens With a Circular Hole

Axial fatigue tests at zero mean stress of 24S-T and 75S-T aluminum-alloy strips with a central circular hole

Published Year

1940-1949 (5) *

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