Nose bluntness and cone angle effects on base pressure and heating in laminar hypersonic flow regime, using free flight telemetry technique


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    Title :

    Free-flight base pressure and heating measurements on sharp and blunt cones in a shock tunnel.


    Contributors:

    Published in:

    Publication date :

    1967-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English