Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer


    Contributors:

    Publication date :

    1954-03-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Performance of Separation Nose Inlets at Mach Number 5.5

    Haefeli, Rudolph C / Bernstein, Harry | NTRS | 1953


    Aerodynamic and acoustic performance of high Mach number inlets

    Lumsdaine, E. / Clark, L. R. / Cherng, J. C. et al. | NTRS | 1977


    Noise suppression with high Mach number inlets

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