A series of flight trials was performed on an F-111C aircraft, tail number A8-132, at the RAAF's Aircraft Research and Development Unit. Data obtained from the tests has been analysed in Air Operations Division to determine the aircraft aerodynamic and control derivatives. In this report the longitudinal and lateral derivatives for the take-off and landing configurations are presented and compared with wind tunnel results.
F-111C Longitudinal and Lateral Aerodynamic Flight Data Analysis for Take-off and Landing Configurations
1996
80 pages
Report
No indication
English
F-111C Flight Data Reduction and Analysis Procedures
NTIS | 1990
|Flight-Estimated Nonlinear Spoiler Aerodynamics of the F-111C Aircraft
British Library Conference Proceedings | 1994
|