Computer program predicts leading-edge thrust for wings of arbitrary planform at supersonic speeds. Methods used in program are based on linearized wing theory. Program first calculates lifting pressures, lift coefficients, drag coefficients, moment coefficients, and lift distributions by using aft-element sensing technique. Next, empirical function calculates set of adjusted pressure-coefficient locations along leading edge. This information is then used to determine limiting value of singularity parameter and value of local leading-edge thrust coefficient.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wing and leading-edge thrust


    Contributors:

    Published in:

    Publication date :

    1980-06-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Wing design with attainable leading-edge thrust considerations

    Carlson, H. W. / Shrout, B. L. / Darden, C. M. | NTRS | 1985


    Wing design with attainable leading-edge thrust considerations

    CARLSON, H. W. / SHROUT, B.L. / DARDEN, C. M. | AIAA | 1985


    Improved Method for Prediction of Attainable Wing Leading-Edge Thrust

    Carlson, Harry W. / McElroy, Marcus O. / Lessard, Wendy B. et al. | NTRS | 1996


    Improved Method for Prediction of Attainable Wing Leading-Edge Thrust

    H. W. Carlson / M. O. Mcelroy / W. B. Lessard et al. | NTIS | 1996


    Wing leading-edge device and a wing having such a wing leading-edge device

    BENSMANN STEFAN / ERBAN MARCUS / FEES MARTIN | European Patent Office | 2023

    Free access