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Volumn 14, Issue 1-2, 1999, Pages 179-187

Probabilistic evaluation of fuselage-type composite structures

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPOSITE MATERIALS; COMPUTER SIMULATION; FUSELAGES; PROBABILITY DISTRIBUTIONS; STRAIN; STRESSES;

EID: 0032757449     PISSN: 02668920     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0266-8920(98)00027-7     Document Type: Review
Times cited : (45)

References (7)
  • 3
    • 0022269651 scopus 로고
    • Demonstration of a new, fast probability integration method for reliability analysis
    • Burnside OH, Parr CH, editors. New York: ASME
    • Wu YT. Demonstration of a new, fast probability integration method for reliability analysis. In: Burnside OH, Parr CH, editors. Advances in aerospace structural analysis. New York: ASME, 1985:63-73.
    • (1985) Advances in Aerospace Structural Analysis , pp. 63-73
    • Wu, Y.T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.