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.


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    Title :

    CESSNA Citation II Flight Tests. Flight Test Execution, Elementary Data Processing and Aerodynamic Model Identification


    Contributors:

    Publication date :

    1997


    Size :

    198 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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