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Volumn 19, Issue , 2007, Pages 13102-13119

Automatic transition prediction for RANS computations applied to a generic high-lift wing

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATION; BOUNDARY LAYERS; PROJECT MANAGEMENT; STABILITY; THREE DIMENSIONAL; WINGS;

EID: 34347223597     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1086     Document Type: Conference Paper
Times cited : (18)

References (20)
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  • 4
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    • Numerical Aspects of Transition Prediction for Three-Dimensional Configurations
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  • 6
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  • 7
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    • Transitional Flow Modeling and Application to High-Lift Multi-Element Airfoil Configurations
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    • A. Krumbein, Transitional Flow Modeling and Application to High-Lift Multi-Element Airfoil Configurations, Journal of Aircraft, Vol. 42, pp. 1150-1164, September-October 2005
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  • 8
    • 7544232510 scopus 로고    scopus 로고
    • Transition on a High-Lift Swept Wing in the European Project EUROLIFT
    • Sept
    • J. Perraud, A. Séraudie, F. Moens, Transition on a High-Lift Swept Wing in the European Project EUROLIFT, Journal of Aircraft, Vol. 41(5), pp 1183-1190, Sept. 2004
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    • Perraud, J.1    Séraudie, A.2    Moens, F.3
  • 9
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    • Compressible Laminar Boundary Lavers With Suction on Swept and Tapered Wings
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  • 10
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    • Method of characteristics for computing three-dimensional boundary lavers
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  • 11
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  • 13
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  • 14
    • 34250796126 scopus 로고    scopus 로고
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  • 16
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  • 17
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  • 18
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.