Two NACA wind tunnels completed, 10- by 14-in. supersonic tunnel and supersonic free flight tunnel, both capable of providing test Mach numbers well in excess of 5; in supersonic free flight tunnel high Mach numbers are obtained by firing models at high speed into oncoming supersonic stream; design and operation of equipment.


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    Title :

    Hypersonic research facilities at Ames aeronautical laboratory


    Additional title:

    J Applied Physics


    Contributors:

    Published in:

    Publication date :

    1950


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :