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)
Mesure des Derivees Aerodynamiques en Soufflerie et en Vol (Measurement of Aerodynamic Derivatives in Wind Tunnel and in Flight)
1961
57 pages
Report
Keine Angabe
Englisch
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