Within the disciplinary group of Stability and Control, there was demand for accurate flight test data of the TUD/NLR Cessna Citation II Laboratory aircraft. Flight tests were to be performed to provide flight test data which can be used to determine an accurate unsteady aerodynamic model of the aircraft (which can be sued for SIMONA), as well as to provide force and trajectory information for the validation of a Computational Fluid Dynamics (CFD) methods. The parameter identification process with flight test data can be divided in a number of steps. In this report some of the steps will be discussed, such as: Planning and execution of a flight test program, Input design, Elementary Data Processing, Parameter identification.
CESSNA Citation II Flight Tests. Flight Test Execution, Elementary Data Processing and Aerodynamic Model Identification
1997
198 pages
Report
No indication
English
Aircraft , Aerodynamics , Jet & Gas Turbine Engines , Cessna aircraft , Flight tests , Computerized simulation , Data processing , Turbofan aircraft , Mathematical models , Software , Computational fluid dynamics , Theses , Foreign technology , Cessna Citation aircraft , Pratt and Whitney JT15D-4 engine
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