A Correlation between Flight-determined Longitudinal and Lateral Derivatives and Wind Tunnel Data for the Pilatus PC 9/A Training Aircraft in Approach and Departure Configurations

A Correlation between Flight-determined Longitudinal and Lateral Derivatives and Wind Tunnel Data for the Pilatus PC 9/A Training Aircraft in Approach and Departure Configurations

A series of flight tests were conducted on the PC 9/A aircraft, A23-045, at the Royal Australian Air Force's Aircraft Research and Development Unit. System identification techniques were applied to the data obtained from these flight tests to determine the stability and control derivatives of t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VAN Bronswijk, Nick, Snowden, Andrew D, Keating, Hilary A, Brian, Geoff J
Format: Report
Sprache:eng
Schlagworte:
AERODYNAMIC CONFIGURATIONS
AERODYNAMIC STABILITY
Aerodynamics
AIRCRAFT LANDINGS
APPROACH
AQ F01-06-1117
AUSTRALIA
CONTROL
FLIGHT TESTING
FOREIGN REPORTS
LOGITUDINAL STABILITY
PC 9/A AIRCRAFT
SYSTEM IDENTIFICATION
TAKEOFF
Training Aircraft
WIND TUNNEL TESTS
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Beschreibung
Zusammenfassung:A series of flight tests were conducted on the PC 9/A aircraft, A23-045, at the Royal Australian Air Force's Aircraft Research and Development Unit. System identification techniques were applied to the data obtained from these flight tests to determine the stability and control derivatives of the aircraft. The longitudinal and lateral results for the aircraft in approach and departure configurations are presented in this report and comparisons are made with wind tunnel estimates. --Original contains color plates: All DTIC reproductions will be in black and white.