Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens /
Stress ratio effects on fatigue crack growth in sheet aluminum alloys
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Corporate Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. : [Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information,
1969]
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Series: | NASA technical note ;
D-5390 |
Subjects: |