Described is boundary estimation method of aircraft aerodynamic parameters which allows to determine with sufficient accuracy aerodynamic coefficients, necessary for diagnosis of available aeronautical engineering and for prediction of new real speciments


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    Title :

    Application of boundary estimation method for determining aircraft aerodynamic parameters




    Publication date :

    2000




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




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