Investigation at NACA Lewis Laboratory to study variations of external pressure distributions and wave drags with fineness ratio, Mach number, and area ratio; results intended to serve as guide in design of external contours for supersonic nose inlets and to provide basis for estimating wave drag to be expected from inlets.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Jack, J.R. (author)


    Publication date :

    1950


    Size :

    35 pages


    Remarks:

    Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :