A suggestion for systematic load interaction studies on fatigue crack growth
暂无分享,去创建一个
[1] Rosenfeld. Damage Tolerance in Aircraft Structures , 1971 .
[2] J. Willenborg,et al. A Crack Growth Retardation Model Using an Effective Stress Concept , 1971 .
[3] W. Elber. The Significance of Fatigue Crack Closure , 1971 .
[4] J. Schijve. Fatigue damage accumulation and incompatible crack front orientation , 1972 .
[5] O. E. Wheeler. Spectrum Loading and Crack Growth , 1972 .
[6] R. Roberts,et al. Effect of multiple overloads on fatigue crack propagation in 2024-T3 aluminum alloy , 1973 .
[7] R. Wei,et al. A study of crack closure in fatigue , 1974 .