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    Title :

    The effect of geometry on the base pressure recovery of segmented blunt trailing edges


    Contributors:

    Published in:

    The aeronautical journal ; 98 , 977 ; 267-274


    Publication date :

    1994



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.50 / 55.60
    Local classification TIB:    275/7040





    Flow-around airfoils with blunt, round, and sharp trailing edges

    THOMPSON, B. E. / WHITELAW, J. H. | AIAA | 1988


    Experimental and theoretical study of wings with blunt trailing edges

    RAMJEE, V. / TULAPURKARA, E. G. / BALABASKARAN, V. | AIAA | 1986


    Effect of surface grooves on base pressure for a blunt trailing-edgeairfoil

    SELBY, GREGORY V. / MIANDOAB, FARID H. | AIAA | 1990