Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Calculation of pressure on slender airplanes in subsonic and supersonic flow


    Additional title:

    NACA -- Tech Note


    Contributors:
    Heaslet, M.A. (author) / Lomax, H. (author)


    Publication date :

    1953


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English