A wind tunnel test of a dynamically scaled aircraft model equipped with sensors and actuators is presented. The dynamic response was compared with the result of a computer simulation. A good correlation is obtained after adjustment of the dynamic derivatives. The natural dynamic behavior of the model was changed in order to simulate different aircraft in different missions.
Flight-Mechanics Test with a Restricted Flying Aircraft Model in a Wind Tunnel
1985
151 pages
Report
Keine Angabe
Englisch
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