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.
Comparison of Aerodynamic Coefficients Obtained from Theoretical Calculations Wind Tunnel Tests and Flight Tests Data Reduction for the Alpha Jet Aircraft
1980
31 pages
Report
No indication
English
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