Design of nozzles for high Mach number tunnels.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to nozzle of square test section


    Additional title:

    NACA -- Tech Note


    Contributors:
    Beckwith, I.E. (author) / Ridyard, H.W. (author) / Cromer, N. (author)


    Publication date :

    1952


    Size :

    30 pages


    Remarks:

    Charts, Tables


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :