Effects of Compressive Overloads on Fatigue Crack Growth
- 1 February 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 12 (2) , 100-104
- https://doi.org/10.2514/3.59807
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- On the influence of single and multiple peak overloads on fatigue crack propagation in 7075-T6511 aluminumEngineering Fracture Mechanics, 1973
- Effect of Multiple Overloads on Fatigue Crack Propagation in 2024-T3 Aluminum AlloyPublished by ASTM International ,1973
- Overload Effects on Subcritical Crack Growth in Austenitic Manganese SteelPublished by ASTM International ,1973
- Method of analysis and prediction for variable amplitude fatigue crack growthEngineering Fracture Mechanics, 1972
- Fatigue Crack Growth in Notched Parts With Compressive Mean LoadJournal of Basic Engineering, 1972
- Spectrum Loading and Crack GrowthJournal of Basic Engineering, 1972
- Effects of Tension-Compression Cycling on Fatigue Crack Growth in High Strength AlloysJournal of Engineering for Industry, 1971
- A Crack Growth Retardation Model Using an Effective Stress ConceptPublished by Defense Technical Information Center (DTIC) ,1971
- Crack Growth Under Cyclic CompressionJournal of Basic Engineering, 1969
- Effect of stress ratio on fatigue-crack growth in 7075-T6 aluminum-alloy sheetEngineering Fracture Mechanics, 1969