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Volumn 39, Issue 1, 2002, Pages 167-174

Equivalent level of safety approach to damage-tolerant aircraft structural design

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED DESIGN; PROBABILITY; SAFETY FACTOR; STATISTICAL METHODS; STRENGTH OF MATERIALS;

EID: 0036181173     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2911     Document Type: Article
Times cited : (14)

References (11)
  • 1
    • 0005899890 scopus 로고    scopus 로고
    • Development of probabilistic design methodology for composite structures
    • Federal Aviation Administration, DOT/FAA/AR-95/17, Washington, DC, Aug.
    • (1997)
    • Gray, P.M.1    Riskalla, M.G.2
  • 2
    • 0008517852 scopus 로고    scopus 로고
    • Probabilistic design methodology for composite aircraft structures
    • Federal Aviation Administration, DOT/FAA/AR-99/2, Washington, DC, June
    • (1999)
    • Long, M.W.1    Narciso, J.D.2
  • 4
    • 85037311930 scopus 로고    scopus 로고
    • Probabilistic design of damage tolerant composite aircraft structures (ProDeCompoS); final report under annex 1 to memorandum of cooperation AIA/CA-71 between the federal aviation administration (FAA) and the central aerohydrodynamic institute (TsAGI)
    • Central Aerohydrodynamic Inst., Moscow
    • (1996)
    • Ushakov, A.1    Kuznetsov, A.2    Stewart, A.3    Mishulin, I.4
  • 5
    • 0008483190 scopus 로고    scopus 로고
    • Structural design methodology based on concepts of uncertainty
    • NASA CR-2000-209847, Langley, VA, Feb.
    • (2000)
    • Lin, K.Y.1    Du, J.2    Rusk, D.T.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.