Influence of fastener holes on residual strength
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Mechanical Failure Analysis and Simulation · Engineering Structural Analysis Methods
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References (10)
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1. P. Tong et al. ‘Structural Integrity of Airframe Structures with MSD', presented at the 3rd Annual International Conference on Aging Aircraft, Federal Aviation Administration, Nov. 1991, Washington D.C.
2. P. Tong, Computers and Structures 19, No. 1–2 (1984) 263–269.10.1016/0045-7949(84)90226-8 ↗
3. S.N. Atluri and P. Tong, in Structural Integrity Analyses of Aging Airplanes, Atluri, Sampath, and Tong (eds), Springer (1991).10.1007/978-3-642-84364-8 ↗
4. P. Tong, Li Chen and R. Greif, ‘Hybrid Finite Element Modeling of Multiple Site Damage of Airframe Structures’, presented at the ICES '91, Melbourne, Australia, August 11–16, 1991.
5. P. Tong, R. Greif, L. Chen and D.Y. Jeong, ‘Damage Tolerance of Fuselage Panels with Widespread Fatigue Damage’, presented at the 17th Symposium of the ICAF, Stockholm, Sweden, June 9–11, 1993.
6. T. Swift, ‘Damage Tolerance Capability’, presented at the Specialists' Conference on Fatigue of Aircraft Materials, Delft, Netherlands, October, 1992.
7. T. Swift, ‘Widespread fatigue Damage Monitoring Issues and Concerns’, presented at the 5th International Conference on Structural Airworthiness of New and Aging Aircraft, Hamburg, Germany, June 16–18, 1993.
8. S.N. Atluri et al., ‘Damage Tolerance of Fuselage Panels with Widespread Fatigue Damage’, presented at the 17th Symposium of the ICAF, Stockholm, Sweden, June 9–11, 1993.
9. J.C. Newman, An Improved Method of Collocation for the Stress Analysis of Cracked Plates with Various Shaped Boundaries, NASA TN D-6376 (1971).
10. M. Isida, Engineering Fracture Mechanics 5 (1973) 647–665.10.1016/0013-7944(73)90045-3 ↗