Analytical procedures used to evaluate the application of suction boundary-layer control (BLC) to subsonic V/STOL inlets are presented. These procedures have been used to analytically predict the optimum (minimum suction power required) location and extent for a suction slot of two different surface resistances within a subsonic V/STOL inlet. Results of this analytical study are presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Analytical study of suction boundary layer control for subsonic V/STOL inlets


    Contributors:
    Boles, M. A. (author) / Ramesh, K. (author) / Hwang, D. P. (author)

    Publication date :

    1984-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Zero-length inlets for subsonic V/STOL aircraft

    GLASGOW, E. R. / BECK, W. E. / WOOLLETT, R. R. | AIAA | 1983


    Zero-length inlets for subsonic V/STOL aircraft

    GLASGOW, E. / BECK, W. / WOOLLETT, R. | AIAA | 1981


    Zero-length inlets for subsonic V/STOL aircraft

    Glasgow, E. R. / Beck, W. E. / Woollett, R. R. | NTRS | 1981