Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effects of Nozzle Exit Geometry on Forebody Vortex Control Using Blowing


    Contributors:

    Published in:

    Publication date :

    1994



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Local classification TIB:    770/7040



    Effects of nozzle exit geometry on forebody vortex control using blowing -

    Gittner, Nathan M. / Chokani, Ndaona | AIAA | 1994




    F-15 forebody vortex flow control using jet nozzle blowing

    Iwanski, Kenneth / O'Rourke, Matthew | AIAA | 1995


    F-15 forebody vortex flow control using jet nozzle blowing

    Iwanski, Kenneth P. / O'Rourke, Matthew J. | AIAA | 1996