The first part of the report, which concerns wind tunnel research on aerodynamic derivatives, amplifies previous overall studies by examining critically the methods and facilities generally used at the present time for such work. Some progress is reported and some results thus made possible are presented. The second part is devoted to flight tests undertaken by a French firm after development of prototype apparatus. (Author)


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    Title :

    Mesure des Derivees Aerodynamiques en Soufflerie et en Vol (Measurement of Aerodynamic Derivatives in Wind Tunnel and in Flight)


    Contributors:
    M. Scherer (author) / P. Mathe (author)

    Publication date :

    1961


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English