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Volumn 39, Issue 1, 2002, Pages 175-180

Residual strength and corrosion rate predictions of aging aircraft panels: Neural network study

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED ANALYSIS; COMPUTER SIMULATION; CORROSION; DETERIORATION; FATIGUE OF MATERIALS; NEURAL NETWORKS; STRENGTH OF MATERIALS;

EID: 0036182074     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2912     Document Type: Article
Times cited : (14)

References (18)
  • 2
    • 0029425801 scopus 로고
    • On the mechanisms of interaction between corrosion and fatigue cracking in aircraft aluminum alloys
    • edited by C. I. Chang and C. T. Sun; American Society of Mechanical Engineers
    • (1995) Structural Integrity of Aging Aircraft , vol.47 AD , pp. 159-169
    • Koch, G.H.1
  • 4
    • 0003876753 scopus 로고    scopus 로고
    • Pre-corroded fastener hole multiple site damage testing
    • EA 96-135 TH-041, KC-135 Fleet Support Contract, F34601-96-C-0111, The Boeing Company, St. Louis, Missouri, Sept.
    • (1998)
    • Luzar, J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.