Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Challenge for Natural Transition Simulation of Wing Boundary Layer with an Innovative 3-D LES Technique



    Conference:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Publication date :

    2006-01-01


    Size :

    AIAA Paper 2006-3533-2006-3538


    Remarks:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Challenge for Natural Transition Simulation of Wing Boundary Layer with an Innovative 3-D LES Technique

    Atobe, Takashi / Kurotaki, Takuji / Sumi, Takahiro et al. | AIAA | 2006


    Direct Numerical Simulation of Transition in a Swept Wing Boundary Layer

    Duan, Lian / Choudhari, Meelan M. / Li, Fei et al. | AIAA | 2013


    Direct Numerical Simulation of Transition in a Swept Wing Boundary Layer

    Duan, L. / Choudhari, M.M. / Li, F. et al. | British Library Conference Proceedings | 2013


    Large-Eddy Simulation of Laminar-Turbulent Transition in a Swept-Wing Boundary Layer

    Huai, X. / Joslin, R. D. / Piomelli, U. et al. | British Library Conference Proceedings | 1997


    Calculation of boundary layer transition of swept wing with suction

    Arai, Nobuyuki / Noto, Kazuo / Hiraoka, Katsumi | AIAA | 2000