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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    Titel :

    Application of boundary estimation method for determining aircraft aerodynamic parameters




    Erscheinungsdatum :

    2000




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




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