A computational system for estimation of nonlinear aerodynamic characteristics of wings at supersonic speeds was developed and was incorporated in a computer program. This corrected linearized theory method accounts for nonlinearities in the variation of basic pressure loadings with local surface slopes, predicts the degree of attainment of theoretical leading edge thrust, and provides an estimate of detached leading edge vortex loadings that result when the theoretical thrust forces are not fully realized.


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    Title :

    Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds


    Contributors:

    Publication date :

    1980-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :