## Abstract Fatigue‐crack‐growth tests were conducted on compact, C(T), specimens made of D16Cz aluminum alloy. Constant‐amplitude tests were conducted over a range of stress ratios (R = P~min~/P~max~ = 0.1 to 0.75). Comparisons were made between test data from middle‐crack tension, M(T), specimens
✦ LIBER ✦
A strip-yield rate-dependent model for rapid loading conditions
✍ Scribed by Fred Nilsson; Patrich Ohlsson; Fredrik Sjöberg; Per Ståhle
- Book ID
- 103070906
- Publisher
- Elsevier Science
- Year
- 1989
- Tongue
- English
- Weight
- 607 KB
- Volume
- 33
- Category
- Article
- ISSN
- 0013-7944
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