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Dtic Ada311534%3a F 111c Longitudinal And Lateral Aerodynamic Flight Data Analysis For Take Off And Landing Configurations. by Defense Technical Information Center
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1DTIC ADA311534: F-111C Longitudinal And Lateral Aerodynamic Flight Data Analysis For Take-off And Landing Configurations.
By Defense Technical Information Center
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.
“DTIC ADA311534: F-111C Longitudinal And Lateral Aerodynamic Flight Data Analysis For Take-off And Landing Configurations.” Metadata:
- Title: ➤ DTIC ADA311534: F-111C Longitudinal And Lateral Aerodynamic Flight Data Analysis For Take-off And Landing Configurations.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA311534: F-111C Longitudinal And Lateral Aerodynamic Flight Data Analysis For Take-off And Landing Configurations.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Snowden, A. D. - DEFENCE SCIENCE AND TECHNOLOGY ORGANIZATION CANBERRA (AUSTRALIA) - *AERODYNAMIC CONFIGURATIONS - *FLIGHT TESTING - *JET FIGHTERS - TAKEOFF - AIRCRAFT MODELS - AUSTRALIA - WIND TUNNELS - AIRCRAFT LANDINGS - AERODYNAMICS.
Edition Identifiers:
- Internet Archive ID: DTIC_ADA311534
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The book is available for download in "texts" format, the size of the file-s is: 39.10 Mbs, the file-s for this book were downloaded 69 times, the file-s went public at Sun Apr 01 2018.
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