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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 Factors of 2.0 and 4.0
Report presenting the results of axial-load fatigue tests on notched specimens of three sheet materials: 24S-T3 and 75S-T6 aluminum alloys and SAE 4130 steel. Fatigue tests were run at several levels of nominal mean stress, including a zero nominal mean stress. Fatigue tests for notched specimens ar
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