A study has been performed to determine the optimum, practical high-energy driver technique to be employed with the Air Force Aero Propulsion Laboratory 120-inch shock tunnel. The aerodynamic performance and engineering design and feasibility of several candidate techniques were investigated. (Author)


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    Title :

    Study of Large, High - Performance Shock Tunnel Drivers


    Contributors:
    C. E. Smith (author) / D. G. Hajjar (author) / W. G. Reinecke (author)

    Publication date :

    1967


    Size :

    83 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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