Study was conducted to ascertain feasibility of facility capable of producing high velocity and high Reynolds number environment; most promising were magnetic annular arc tunnels and expansion tubes as single-stage techniques, and shock tunnel driving j×B accelerator as two-stage technique; results of techniques and devices used are presented; experimental performance of magnetic annular arc implies that it can achieve environment considered, but research directed more specifically to this goal must be performed to fully evaluate its potential.


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    Title :

    Feasibility of high-performance aerodynamic impulse facility


    Additional title:

    AIAA J


    Contributors:
    Leonard, R.L. (author) / Rose, P.H. (author)

    Published in:

    AIAA Journal ; 6 , n 3


    Publication date :

    1968


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





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