Development of unusual test capabilities for arc discharge wind tunnel which has nominal run time of 30 msec; design and test techniques employed, problem areas encountered, and samples of test data obtained for simulation of rocket power effects on vehicle stability and measurement of aerodynamic damping; sample data indicate quality of data obtainable; samples of self-luminous and shadowgraph photographs shown.


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    Title :

    New test techniques for hypervelocity wind tunnel


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1962


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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