Application of fracture mechanics and half-cycle theory to the prediction of fatigue life of aerospace structural components
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Abstract
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Probabilistic and Robust Engineering Design · High Temperature Alloys and Creep
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References (11)
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1. D.R. Donaldson and W.F. Anderson, in Proceedings of the Crack Propagation Symposium, Vol. 2, Cranfield, (September 1961).
2. J.P. Butler, The Material Selection and Structural Development Process for Aircraft Structural Integrity Under Fatigue Conditions. AFFDL-TR-70-144, Conference Proceedings, Air Force Conference, Miami, Florida, December 15?16, 1969.
3. W. Astley and J. Scott, Engineering Practice to Avoid Stress Corrosion Cracking. (The Environment Encountered in Aircraft Service.) AGARD Conference Proceedings No. 53.
4. R.G. Forman, V.E. Kearney and R.M. Engle, Journal of Basic Engineering, Transactions ASME, D89 (1967) 459.10.1115/1.3609637 ↗
5. E.K. Walker, The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum, Effects of Environments and Complex Load History on Fatigue Life. ASTM STP 462 (1970) 1.
6. J. Schijve, Engineering Fracture Mechanics, 11 (1979) 167?221.10.1016/0013-7944(79)90038-9 ↗
7. W.L. Starkey and S.M. Marco, Transactions ASME (1957) 1329?1336.10.1115/1.4013318 ↗
8. C. Incarbone, in Fatigue of Aircraft Structures, Proceedings of the Symposium held in Paris, 16th?18th May 1961, W. Barrois and E.L. Ripley (eds), Pergamon Press, New York (1963) 209?217.
9. S.H. Smith, in Acoustic Fatigue in Aerospace Structures, Syracuse University Press (1965) 331.
10. William L. Ko, Alan L. Carter, William W. Totton and Jules M. Ficke, Application of Fracture Mechanics and the Half-Cycle Method to the Prediction of Fatigue Life of B-52 Aircraft Pylon Components. NASA TM-88277 (1988).
11. William L. Ko and Lawrence S. Schuster, Stress Analyses of B-52 Pylon Hooks. NASA TM-84924 (1985).