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Volumn 37, Issue 2, 2000, Pages 325-331

Strength of 2024-T3 aluminum panels with multiple site damage

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; FATIGUE OF MATERIALS; FRACTURE MECHANICS; MATHEMATICAL MODELS; REGRESSION ANALYSIS; STRENGTH OF MATERIALS; STRUCTURAL PANELS;

EID: 0033894246     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2597     Document Type: Article
Times cited : (32)

References (15)
  • 2
    • 0343225137 scopus 로고    scopus 로고
    • The effect of multiple site damage on the critical strength of aluminum panels
    • Smith, B., Camenzind, J., Myose, R., Saville, P., Mouak, A., and Horn, W., "The Effect of Multiple Site Damage on the Critical Strength of Aluminum Panels," Developments in Theoretical and Applied Mechanics, Vol. 19, 1998, pp. 421-429; also Proceedings of the Nineteenth Southeastern Conference on Theoretical and Applied Mechanics, 1998.
    • (1998) Developments in Theoretical and Applied Mechanics , vol.19 , pp. 421-429
    • Smith, B.1    Camenzind, J.2    Myose, R.3    Saville, P.4    Mouak, A.5    Horn, W.6
  • 5
    • 85037969697 scopus 로고    scopus 로고
    • Improved engineering methods for determining the critical strength of aluminum panels with multiple site damage
    • edited by Charles E. Harris, Langley Research Center, Hampton, VA, Jan. NASA CP-1999-208982
    • Smith, B., Mouak, A., Saville, P., Myose, R., and Horn, W., "Improved Engineering Methods for Determining the Critical Strength of Aluminum Panels with Multiple Site Damage," Proceedings of the Second Joint NASA/FAA/DoD Conference on Aging Aircraft, edited by Charles E. Harris, Langley Research Center, Hampton, VA, Jan. 1999, pp. 525-534; also NASA CP-1999-208982.
    • (1999) Proceedings of the Second Joint NASA/FAA/DoD Conference on Aging Aircraft , pp. 525-534
    • Smith, B.1    Mouak, A.2    Saville, P.3    Myose, R.4    Horn, W.5
  • 8
    • 0343225136 scopus 로고
    • Predicting failure of specimens with either surface cracks or corner cracks at holes
    • June
    • Newman, J. C., Jr., "Predicting Failure of Specimens with Either Surface Cracks or Corner Cracks at Holes," NASA TN D-8244, June 1976.
    • (1976) NASA TN D-8244
    • Newman J.C., Jr.1
  • 12
    • 0004305470 scopus 로고    scopus 로고
    • Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, May
    • Heinimann, M. B., "Analysis of Stiffened Panels with Multiple Site Damage," Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, May 1997.
    • (1997) Analysis of Stiffened Panels with Multiple Site Damage
    • Heinimann, M.B.1
  • 14
    • 0003666084 scopus 로고
    • The effects of multi-site damage on the arrest capability of aircraft fuselage structure
    • TR 9302, Galena, OH, June
    • Broek, D., "The Effects of Multi-Site Damage on the Arrest Capability of Aircraft Fuselage Structure," FractuResearch, TR 9302, Galena, OH, June 1993.
    • (1993) FractuResearch
    • Broek, D.1
  • 15
    • 0343660786 scopus 로고    scopus 로고
    • Residual strength analysis of skin splices with multiple site damage
    • edited by Charles E. Harris, Langley Research Center, Hampton, VA, Jan.
    • Ingram, J. E., Kwon, Y. S., Duffié, K. J., and Irby, W. D., "Residual Strength Analysis of Skin Splices with Multiple Site Damage," Proceedings of the Second Joint NASA/FAA/DoD Conference on Aging Aircraft, edited by Charles E. Harris, Langley Research Center, Hampton, VA, Jan. 1999, pp. 427-436; also NASA CP-1999-208982.
    • (1999) Proceedings of the Second Joint NASA/FAA/DoD Conference on Aging Aircraft , pp. 427-436
    • Ingram, J.E.1    Kwon, Y.S.2    Duffié, K.J.3    Irby, W.D.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.