TY - DATA
T1 - Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection
PY - 2023/06/30
AU - Paul Lancelot
AU - Roeland de Breuker
UR - 
DO - 10.4121/83e60905-b41f-4460-99a0-376487627108.v1
KW - Control surfaces
KW - Transonic aerodynamics
KW - Simulink
KW - Model identification
KW - Unsteady loads
N2 - <p>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. https://doi.org/10.4233/uuid:e37566e8-cb46-4f90-863d-9cfe0b634507"</p><p><br></p>
ER -