Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection



This is an aerodynamic reduced order model (ROM) for Matlab/Simulink. It is applied to the scaled-up (x20) OAT15A airfoil, predicting the incremental lift of an arbitrary dynamic aileron deflection at Mach 0.73. The data contains the model and inputs to reproduce Figure 3.10 from the following PhD Dissertation: "Lancelot, P. M. G. J. (2023). Transonic Wing and Control Surface Loads Modelling for Aeroservoelastic Analysis."
Date made available30 Jun 2023
PublisherTU Delft - 4TU.ResearchData
Date of data production2023 -

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