Fatigue issues in aircraft maintenance and repairs
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Probabilistic and Robust Engineering Design · Advanced Sensor Technologies Research
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References (29)
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1. Whittaker, I. C. and Besuner, P. M., A reliability analysis approach to fatigue life variability of aircraft structures. Air Force Materials Laboratory Technical Report AFML-TR-69-65, April 1969.
2. Whittaker, I. C., Development of titanium and steel fatigue variability model for application of reliability analysis approach to aircraft structures. Air Force Materials Laboratory Technical Report AFML-TR-72-236, October 1972.10.21236/AD0758219 ↗
3. Broek, D., Damage tolerance in practice, AGARD Lecture Series No. 97 on Fatigue Mechanics in Practice. Delft, The Netherlands, October 1978.
4. Craig, L. E. and Goranson, U. G., Airworthiness assessment of Boeing jet transport structures. 10th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Brussels, Belgium, May 1979.
5. Goranson, U. G., Hall, J., Maclin, J. R. and Watanabe, R. T., Long life damage tolerant jet transport structures. ASTM Symposium on Design of Fatigue and Fracture Resistant Structures, November 10–11, 1980.10.1520/STP28854S ↗
6. Galda, K. H., Maintenance system by means of damage tolerance principle. 13th Symposium of the International Committee on Fatigue (ICAF), Pisa, Italy, May 22–24, 1985.
7. Broek, D. Elementary Engineering Fracture Mechanics, 4th edn. Martinus Nijhoff, 1987.10.1007/978-94-009-4333-9 ↗
8. Miller, M., Luthra, V. K. and Goranson, U. G., Fatigue crack growth characterization of jet transport structures. 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Ottawa, Canada, June 8–12, 1987.
9. Swift, T., Damage tolerance in pressurized fuselages. 11th Plantema Memorial Lecture, 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Ottawa, Canada, June 8–12, 1987.
10. Goranson, U. G. and Miller, M., Aging jet transport structural evaluation programs. 15th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Jerusalem, Israel, June 21–23, 1989.10.1007/978-3-642-84364-8_9 ↗
11. Whittaker, I. C., Miller, M. and Goranson, U. G., Durability and damage tolerance evaluations of jet transport structures. 5th International Conference on Structural Safety and Reliability (ICOSSAR), San Francisco, CA, August 1989.
12. Sampath, S. G. and Broek, D., The prospect of detecting and dealing with widespread fatigue damage: threshold for inspecting MSD susceptible lap spices. International Conference on Aircraft Damage Assessment and Repair, Melbourne, Australia, August 26–28, 1991.
13. Whittaker, I. C., Stilwell, P. B. and Sizemore, D. R., Fleet fatigue cracking threshold prediction. 16th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Tokyo, Japan, May 20–24, 1991.
14. Schijve, J., Multiple site fatigue damage of riveted joints. Proceedings of the International Workshop on Structural Integrity of Aging Airplanes, Atlanta, GA, March 31–April 2, 1992.
15. Schmidt, H. J. and Brandecker, B., Results of the AAWG industry committee on widespread fatigue damage. Proceedings of the International Workshop on Structural Integrity of Aging Airplanes, Atlanta, GA, March 31–April 2, 1992.
16. Swift, T., Unarrested fast fracture. Proceedings of the International Workshop on Structural Integrity of Aging Airplanes, Atlanta, GA, March 31–April 2, 1992.
17. Broek, D., The effects of multi-site-damage on the arrest capability of aircraft fuselage structures. FractuREsearch TR9302, June 1993.
18. Goranson, U. G., Damage tolerance facts and fiction. 17th Symposium of the International Committee on Aeronautical Fatigue, Engineering Material Advisory Service Ltd., 17-1 (1993–1996).
19. Thomson, D., Hoadley, D. and McHatton, J., Load tests of flat and curved panels with multiple cracks. Foster–Miller Draft Final Report to the FAA Center, September 1993.
20. Bigelow, C. A. and Tan, P. W., An integrated methodology for assessing widespread fatigue damage in aircraft structures. Proceedings of the FAA–NASA 6th International Conference on the Continued Airworthiness of Aircraft Structures, Atlantic City, NJ, June 27–28, 1995, pp. 121–138.
21. deWit, R., Fields, R. J., Low III, S. R., Harne, D. E. and Foecke, T., Fracture testing of large-scale thin-sheet aluminum alloy. NIST Report 5661, Prepared for FAA, May 1995.10.6028/NIST.IR.5661 ↗
22. Aging aircraft airworthiness initiatives10.1299/jsmemag.98.915_101 ↗
23. Gruber, M. L., Mazur, C. J., Wilkins, K. E. and Worden, R. E., Investigation of fuselage structure subject to widespread fatigue damage. Final Report to the FAA, DOT/FAA/AR-95/47, October 1995.
24. Harris, C. E., Starnes Jr., J. H. and Newman Jr., J. C., Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures. Proceedings of the FAA–NASA 6th International Conference on the Continued Airworthiness of Aircraft Structures, Atlantic City, NJ, June 27–28, 1995, pp. 139–164.
25. Newman Jr., J. C. and Dawicke, D. S., Fracture analysis of stiffened panels under biaxial loading with widespread cracking. NASA Report TM 110197, November 1995.
26. Wang, L., Brust, F. W. and Atluri, S. N., Computational predictions of the NIST multiple site damage experimental results. FAA Center of Excellence Report, Georgia Institute of Technology, August 1995.
27. McGuire, J. F. and Varanasi, S. R., Boeing structural design and technology improvements. The Boeing Airliner, April–June 1996.
28. Gruber, M. L., Wilkins, K. E. and Worden, R. E., Investigation of fuselage structure subject to widespread fatigue damage. Proceedings of the FAA–NASA Symposium on Continued Airworthiness of Aircraft Structures, Atlanta, GA, August 1996.
29. Whittaker, I. C. and Chen, H. C., Widespread fatigue damage threshold estimates. Proceedings of the FAA–NASA Symposium on Continued Airworthiness of Aircraft Structures, Atlanta, GA, August 1996.