Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    An Investigation of Three Transonic Fuselage Air Inlets at Mach Numbers from 0.4 to 0.94 and at a Mach Number of 1.19


    Contributors:

    Publication date :

    1950-11-07


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



    Noise suppression with high Mach number inlets

    Lumsdaine, Edward / Cherng, Jenn G. / Tag, Ismail | TIBKAT | 1976



    Multibody interference at transonic Mach numbers

    CHAPMAN, GARY / BONNESS, WILLIAM / LYNCH, PRISCA | AIAA | 1992


    Preliminary Investigation at Mach Number 1.9 of Simulated Wing-root Inlets

    Piercy, Thomas G / Weinstein, Maynard I | NTRS | 1955