Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft
Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft
Longitudinal and lateral-directional estimates of the aerodynamic derivatives of the X-24B research aircraft were obtained from flight data by using a modified maximum likelihood estimation method. Data were obtained over a Mach number range from 0.35 to 1.72 and over an angle of attack range from 3.5 deg. to 15.7 deg. Data are presented for a subsonic and transonic configuration. The flight derivatives were generally consistent and documented the aircraft well. The correlation between the flight data and wind-tunnel predictions is presented and discussed.
Dokumentinformationen
Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft
1997
70 pages
Report
Keine Angabe
Englisch
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