The nature of some cases of flow separation, flow-field interference, unusual vehicle shape or size, excessive deviations to high angular positions. Mach number induced effects, Reynolds number effects, and effects of protruberances on wind tunnel investigations of sounding rockets are illustrated.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Role of Wind Tunnels in Predicting Sounding Rocket Aerodynamics


    Contributors:

    Publication date :

    1983


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English