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Volumn 27, Issue 3, 1997, Pages 237-253

Fracture mechanics of plates and shells applied to fail-safe analysis of fuselage Part II: Computational results

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); CALCULATIONS; CRACKS; FINITE ELEMENT METHOD; FUSELAGES; PLATES (STRUCTURAL COMPONENTS); SHEAR DEFORMATION; SHELLS (STRUCTURES); STIFFNESS;

EID: 0031202584     PISSN: 01678442     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-8442(97)00025-6     Document Type: Article
Times cited : (2)

References (9)
  • 5
    • 0002577646 scopus 로고
    • Damage Tolerance in Pressurized Fuselages
    • New Material and Fatigue Resistant Aircraft Design, Ottawa, Canada, June 10-12
    • T. Swift, Damage Tolerance in Pressurized Fuselages, 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF), New Material and Fatigue Resistant Aircraft Design, Ottawa, Canada, June 10-12, 1987.
    • (1987) 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF)
    • Swift, T.1
  • 7
    • 0016872746 scopus 로고
    • A degenerate solid element for linear fracture analysis of plate bending and general shells
    • R.S. Barsoum, A degenerate solid element for linear fracture analysis of plate bending and general shells, Int. J. Numer. Methods Eng. 10 (1976) 551-564.
    • (1976) Int. J. Numer. Methods Eng. , vol.10 , pp. 551-564
    • Barsoum, R.S.1
  • 8
    • 0027877950 scopus 로고
    • Some computational tool for the analysis of through cracks in stiffened fuselage shells
    • C.C. Rankin, F.A. Brogan, E. Riks, Some computational tool for the analysis of through cracks in stiffened fuselage shells, Comput. Mech. 13 (1993) 143-156.
    • (1993) Comput. Mech. , vol.13 , pp. 143-156
    • Rankin, C.C.1    Brogan, F.A.2    Riks, E.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.