Aerodynamic data from NASA Ames Research Center's 11-Foot Transonic Wind Tunnel are plotted for the 1/8-scale X-29A forward-swept wing aircraft model. Eleven configurations were tested to provide supplemental data to investigate single surface failure modes, complex nonlinearities, and model buildup. These data can be used for control system refinements, pilot training, flight planning, and aerodynamic model validation. Data are presented as corrected wind tunnel data without analysis to document results that are being used for the aerodynamic model.
X-29A Longitudinal and Directional Force and Moment Supplemental Transonic Wind Tunnel Test Results
1984
289 pages
Report
Keine Angabe
Englisch
NACA transonic wind-tunnel test sections
TIBKAT | 1955
|NACA transonic wind-tunnel test sections
Engineering Index Backfile | 1955
|NACA transonic wind tunnel test sections
SLUB | 1956
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