naca-tn-2639
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- January 17, 2017 Create Date
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National Advisory Committee for Aeronautics, Technical Notes - 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 1.5
| File | Action |
|---|---|
| naca-tn-2639 Fatigue Strengths of Aircraft Materials Axial Load Fatigue Tests on Notched Sheet Specimens of 24S-T3 and.pdf | Download |
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