Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effect of Reynolds number on the aerodynamic stability and control characteristics of 55° clipped-delta-wing orbiter configuration at supersonic Mach numbers


    Contributors:


    Publication date :

    1976


    Size :

    95 S.


    Remarks:

    Ill., graph. Darst


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English