Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fitting


    Contributors:
    VADYAK, J. (author) / HOFFMAN, J. (author) / BISHOP, A. (author)

    Conference:

    17th Aerospace Sciences Meeting ; 1979 ; New Orleans , LA , U.S.A.



    Publication date :

    1979-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English