A numerical method for the estimation of leading edge thrust for supersonic wings of arbitrary planform was developed and was programmed as an extension to an existing high speed digital computer method for prediction of wing pressure distributions. The accuracy of the method was assessed by comparison with linearized theory results for a series of flat delta wings. Application of the method to wings of arbitrary planform, both flat and cambered, is illustrated in several examples.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Estimation of leading-edge thrust for supersonic wings of arbitrary planform


    Contributors:

    Publication date :

    1978-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Estimation of leading-edge thrust for supersonic wings of arbitrary plabform

    Carlson, Harry W. / Mack, Robert J. | TIBKAT | 1978



    Supersonic wings with significant leading-edge thrust at cruise

    Robins, A. W. / Carlson, H. W. / Mack, R. J. | NTRS | 1980


    Supersonic Wings with Significant Leading-Edge Thrust at Cruise

    A. W. Robins / H. W. Carlson / R. J. Mack | NTIS | 1980