Facility at Ames Laboratory in which aerodynamic models are gun launched in direction opposite to air stream; test Mach numbers up to 10 attained.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Free-flight wind tunnel for aerodynamic testing at hypersonic speeds


    Additional title:

    NACA -- Report


    Contributors:
    Seiff, A. (author)


    Publication date :

    1955


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :