Nose bluntness and angle of attack effects on hypersonic flow, noting shock wave deflection decrease of minimum possible shock angle, varying specific heat ratio, convective heating, boundary layer transition, etc


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of angle of attack and nose bluntness on the hypersonic flow over cones.


    Contributors:

    Publication date :

    1966-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English