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    Title :

    AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT



    Conference:

    International congress; 26th, International Council of the Aeronautical Sciences; 8th AIAA Aviation Technology, Integration, and Operations (ATIO) ; 2008 ; Anchorage, Alaska



    Publication date :

    2008-01-01


    Size :

    79 pages


    Remarks:

    Held on CD-ROM. Also Known as ICAS 2008; Held in e-store (RMS)



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    An Experimental and Computational Study of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat

    Genc, M. / Lock, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008




    Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number

    Genç, M S / Kaynak, Ü / Lock, G D | SAGE Publications | 2009