메뉴 건너뛰기




Volumn 190, Issue 24-25, 2001, Pages 3121-3146

A linearized method for the frequency analysis of three-dimensional fluid/structure interaction problems in all flow regimes

Author keywords

Aeroelasticity; Eigen analysis; Fluid structure interaction; Second order Jacobian

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; SUPERSONIC FLOW; TRANSONIC FLOW;

EID: 0035793731     PISSN: 00457825     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7825(00)00385-6     Document Type: Article
Times cited : (74)

References (29)
  • 17
    • 0030245214 scopus 로고    scopus 로고
    • Development of a finite element aeroelastic analysis capability
    • (1996) J. Aircraft , vol.33 , pp. 995-1002
    • Gupta, K.K.1
  • 18
    • 0015160179 scopus 로고
    • An approximate true damping solution of the flutter equation by determinant iteration
    • (1971) J. Aircraft , vol.8 , pp. 885-889
    • Hassig, H.1
  • 20
    • 2442433925 scopus 로고
    • Towards the ultimate conservative difference scheme V: A second-order sequel to Godounov's method
    • (1979) J. Comput. Phys , vol.32 , pp. 361-370
    • Van Leer, B.1
  • 25
    • 2942757053 scopus 로고
    • Approximate Reimann solvers, parameters vectors and difference schemes
    • (1981) J. Comput. Phys , vol.43 , pp. 357-371
    • Roe, P.L.1
  • 29
    • 0003345196 scopus 로고
    • Agard standard aeroelastic configuration for dynamic response, candidate configuration i. - wing 445.6
    • (1987) NASA TM100492
    • Yates, E.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.