Residual strength of aging aircraft with multiple site damage/multiple element damage

AIAA Journal

Volumn 36, Issue 5, 1998, Pages 840-847

  Wang, L ^a   Chow, W T ^b   Kawai, H ^b   Atluri, S N ^b,c,d  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^c University of California   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0008496766     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.445     Document Type: Article

References (11)

1. Atluri, S. N., Structural Integrity and Durability, Tech Science Press, 1997.
2. Maclin, J. R., "Performance of Fuse;age Pressure Structure," International Conference on Aging Aircraft and Structural Airworthiness, NASA CP 3160, 1991, pp. 67-74.
3. Swift, T., "Widespread Fatigue Damage Monitoring - Issues and Concerns," Proceedings of the 5th International Conference on Structural Airworthiness of New and Aging Aircraft, Washington, DC, 1993, pp. 133-150.
4. Jeong, D. Y., and Tong, P., "Threshold of Multiple Site Damage in Aging Airplanes," Structural Integrity in Aging Aircraft, ASME-AD Vol. 47, American Society of Mechanica; Egineers, New York, 1995, pp. 63-71.
5. Swift, T., "Effect of MSD on Large Damage Residual Strength," Contemporary Research in Engineering Science, edited by R. C. Batra, 1995, pp. 516-539.
6. Wang, L., Brust, F. W., and Atluri, S. N., "The Elastic-Plastic Finite Element Alternating Method and the Prediction of Fracture Under WFD Conditions in Aircraft Structures," Computational Mechanics, Vol. 19, No. 5, 1997, pp. 356-369.
7. Wang, L., Brust, F. W., and Atluri, S. N.,"The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the Prediction of Fracture Under WFD Conditions in Aircraft Structures. Part II. Fracture and the T*-Integral Parameter," Computational Mechanics, Vol. 19, No. 5, 1997, pp. 370-379.
8. Wang, L., Brust, F. W., and Atluri, S. N., "The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the Prediction of Fracture Under WFD Conditions in aircraft Structures. Part III. Computational Predictions of the NIST Multiple Site Damage Experimental Results," Computational Mechanics, Vol. 20, No. 3, 1997, pp. 199-212.
9. Atluri, S. N., Computational Methods in the Mechanics of Fracture, North-Holland, Amsterdam; also translated into Russian, Mir, Moscow, 1986.
10. Wang, L., and Atluri, S. N.,"Recent Advances in the Alternating Method for Elastic and Inelastic Fracture Analysis," Computational Methods in Applied Mechanical Engineering, Vol. 137, No. 1, 1996, pp. 1-58.
11. swift, T., "Fracture Analysis of Stiffened Structures," Damage Tolerance of Metallic Structures, ASTM STP 842, American Society for Testing and Materials, 1984, pp. 69-107.