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

Bibliographic Details
Main Author: Hudson, C. M
Corporate Authors: United States National Aeronautics and Space Administration, Langley Research Center
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]
Series:NASA technical note ; D-5390
Subjects:

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Call Number: NASA TN D-5390

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Call Number: NASA TN D-5390