The report discusses the methods by which aerodynamic coefficients are determined. These include: calculations, wind tunnel experiments and experiments in flight for various prototypes of the Alpha Jet. A comparison of obtained results shows good correlation between expectations and in-flight test results.


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    Title :

    Comparison of Aerodynamic Coefficients Obtained from Theoretical Calculations Wind Tunnel Tests and Flight Tests Data Reduction for the Alpha Jet Aircraft


    Contributors:
    R. Guiot (author) / H. Wunnenberg (author)

    Publication date :

    1980


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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