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Volumn 38, Issue 4, 2001, Pages 628-635

CFD-based aeroelastic eigensolver for the subsonic, transonic, and supersonic regimes

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; DAMPING; EIGENVALUES AND EIGENFUNCTIONS; INVERSE PROBLEMS; ITERATIVE METHODS; LINEARIZATION; PROBLEM SOLVING; SUBSONIC FLOW; SUPERSONIC FLOW; TIME DOMAIN ANALYSIS; TRANSONIC FLOW;

EID: 0035390399     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2839     Document Type: Article
Times cited : (14)

References (30)
  • 8
    • 0015160179 scopus 로고
    • An approximate true damping solution of the flutter equation by determinant iteration
    • (1971) Journal of Aircraft , vol.8 , Issue.11 , pp. 885-889
    • Hassig, H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.