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Volumn 2005, Issue , 2005, Pages 209-222

Toward a computational framework for rotorcraft multi-physics analysis: Adding computational aerodynamics to multibody rotor models

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE; PROBLEM SOLVING; SYNCHRONIZATION; WAKES;

EID: 33745575392     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (16)

References (28)
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  • 9
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    • April
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    • Bauchau, O.A.1    Kang, N.K.2
  • 12
    • 0042813620 scopus 로고    scopus 로고
    • Is there a difference between aeroacustics and aerodynamics? An aeroelastician's view-point
    • Luigi Morino. Is there a difference between aeroacustics and aerodynamics? An aeroelastician's view-point. AIAA Journal, 41(7)1209-1223, 2003.
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    • Morino, L.1
  • 14
    • 0035479802 scopus 로고    scopus 로고
    • Singularities in BIE's for Laplace's equation: Joukowski trailing-edge conjecture revisited
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    • Morino, L.1    Bernardini, G.2
  • 15
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    • Large-scale structures and growth of a flat plate compressible wake
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    • Gai, S.L.1    Hughes, D.P.2    Perry, M.S.3
  • 17
    • 0032053181 scopus 로고    scopus 로고
    • Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and energy conservation, optimal discretization, and application to aeroelasticity
    • Charbel Farhat, Michael Lesoinne, and P. Le Tallec. Load and motion transfer algorithms for fluid/structure interaction problems with non-matching discrete interfaces: Momentum and energy conservation, optimal discretization, and application to aeroelasticity. Computer Methods in Applied Mechanics and Engineering, 157:95-114, 1998.
    • (1998) Computer Methods in Applied Mechanics and Engineering , vol.157 , pp. 95-114
    • Farhat, C.1    Lesoinne, M.2    Le Tallec, P.3
  • 21
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  • 22
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    • NASA, October
    • William Bousman, Colin Young, Francois Toulmay, Neil Gilbert, Strawn Roger, Judith Miller, Thomas Maier, Michel Costes, and Philippe Beaumier. A comparison of lifting-line and CFD methods with flight test data from a research Puma helicopter. TM 110421, NASA, October 1996.
    • (1996) TM 110421
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.