The identification of multi-input, single output linear static models from flight test data is discussed. Models based on least squares are considered. Wind tunnel scale model and flight test data on a propeller slipstream are compared. Dynamic flight test data were analyzed by reconstructing the flight path and forming a data base for the identification of aerodynamic models. Given the relatively low Reynolds number of the wind tunnel experiments, a reasonable correspondence exists between the dynamic flight test results and model predictions.
Aerodynamic Model Identification from Dynamic Flight Test Data and Wind Tunnel Experiments
1982
23 pages
Report
Keine Angabe
Englisch
Model wind tunnel virtual flight test aerodynamic coefficient measurement method
Europäisches Patentamt | 2022
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