Accession Number : ADA311534

Title :   F-111C Longitudinal and Lateral Aerodynamic Flight Data Analysis for Take-off and Landing Configurations.

Descriptive Note : Technical rept.,

Corporate Author : DEFENCE SCIENCE AND TECHNOLOGY ORGANIZATION CANBERRA (AUSTRALIA)

Personal Author(s) : Snowden, A. D. ; Drobik, J. S.

PDF Url : ADA311534

Report Date : APR 1996

Pagination or Media Count : 73

Abstract : 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.

Descriptors :   *AERODYNAMIC CONFIGURATIONS, *FLIGHT TESTING, *JET FIGHTERS, TAKEOFF, AIRCRAFT MODELS, AUSTRALIA, WIND TUNNELS, AIRCRAFT LANDINGS, AERODYNAMICS.

Subject Categories : Aerodynamics
      Attack and Fighter Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE