The concepts, analytical tools, and experimental data available for designing inlets for powered lift aircraft are discussed. It is shown that inlets can be designed to meet noise, distortion, and cruise drag requirements at the flight and engine operating conditions of a powered lift aircraft. The penalty in pressure recovery for achieving the required noise suppression was 0.3 percent.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Inlet technology for powered-lift aircraft


    Contributors:


    Publication date :

    1976-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Powered-lift aircraft technology

    Deckert, W. H. / Franklin, J. A. | NTRS | 1989


    Powered-Lift Aircraft Technology

    W. H. Deckert / J. A. Franklin | NTIS | 1989



    Takeoff predictions for powered-lift aircraft

    Wardwell, Douglas A. / Sandlin, Doral R. / Hahn, Andrew S. | NTRS | 1986