Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection
收藏DataCite Commons2023-06-30 更新2024-07-03 收录
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https://data.4tu.nl/datasets/83e60905-b41f-4460-99a0-376487627108
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资源简介：
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"<br>
提供机构：
4TU.ResearchData
创建时间：
2023-06-30
