The development and evaluation of a semi empirical method to predict pressure distributions on a deformed wing by using an experimental data base in addition to a linear potential flow solution is described. The experimental data accounts for the effects of aeroelasticity by relating the pressures to a parameter which is influenced by the deflected shape. Several parameters were examined before the net leading edge suction coefficient was selected as the best.


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    Title :

    Aeroelastic Loads Prediction for an Arrow Wing. Task 2: Evaluation of Semi-Empirical Methods


    Contributors:
    A. C. Wery (author) / R. M. Kulfan (author) / M. E. Manro (author)

    Publication date :

    1983


    Size :

    123 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English