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Volumn , Issue , 2001, Pages

A finite element/modal technique for nonlinear plate and stiffened panel response prediction

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVE TRANSMISSION; AERODYNAMICS; NONLINEAR ANALYSIS; REGRESSION ANALYSIS; STRESS-STRAIN CURVES; STRUCTURAL PANELS; TIME DOMAIN ANALYSIS;

EID: 85067318902     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1595     Document Type: Conference Paper
Times cited : (45)

References (10)
  • 1
    • 0012864870 scopus 로고
    • Review of Sonic Fatigue Technology
    • B. L. Clarkson, Review of Sonic Fatigue Technology NASA CR-4587. 1994.
    • (1994) NASA CR-4587
    • Clarkson, B.L.1
  • 2
    • 0027693852 scopus 로고
    • Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
    • R. D. Blevins, I. Holehouse and K. R. Wentz., Thermoacoustic loads and fatigue of hypersonic vehicle skin panels Journal of Aircraft 30, 971-978. 1993.
    • (1993) Journal of Aircraft , vol.30 , pp. 971-978
    • Blevins, R.D.1    Holehouse, I.2    Wentz, K.R.3
  • 4
    • 0028196246 scopus 로고
    • Nonlinear response and sonic fatigue of national aerospace space plane surface panels
    • R. Vaicaitis., Nonlinear response and sonic fatigue of national aerospace space plane surface panels Journal of Aircraft 31 10-18. 1994.
    • (1994) Journal of Aircraft , vol.31 , pp. 10-18
    • Vaicaitis, R.1
  • 5
    • 0015301180 scopus 로고
    • Nonlinear acoustic response analysis of plates using the finite element method
    • C. Hwang and W. S. Pi., Nonlinear acoustic response analysis of plates using the finite element method AIAA Journal 10 276-281. 1972.
    • (1972) AIAA Journal , vol.10 , pp. 276-281
    • Hwang, C.1    Pi, W.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.