Transonic unsteady non-linear aerodynamic model predicting the incremental lift of an aileron arbitrary deflection
收藏4TU.ResearchData2023-06-30 更新2026-04-23 收录
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https://data.4tu.nl/datasets/83e60905-b41f-4460-99a0-376487627108/1
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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>
本数据集为适用于Matlab/Simulink的气动降阶模型（Reduced Order Model，ROM）。该模型针对放大20倍的OAT15A翼型，可预测马赫数0.73工况下任意动态副翼偏转对应的增量升力。本数据集包含可复现下述博士学位论文中图3.10的模型与输入参数：Lancelot, P. M. G. J. (2023). 《用于气动伺服弹性分析的跨声速机翼与操纵面载荷建模》. https://doi.org/10.4233/uuid:e37566e8-cb46-4f90-863d-9cfe0b634507
创建时间：
2023-06-30
