Datasheet-Experimental and Computational Strategies for Improving the Aerodynamic Performance with SETE

Paper Title: Experimental and Computational Strategies for Improving The Aerodynamic Performance with SETE Paper Abstract: An open-loop wind tunnel experiment and Computational Fluid Dynamics simulations are carried out on several Static Extended Trailing Edge (SETE) attached to the NACA0012 airfoil wing model to investigate the effect of a SETE on the aerodynamic characteristics at low Reynolds. A thin extended trailing edge of length 20% of the chord and 15° deflection appears to generate 74.24% more lift concerning the baseline model. SETE enables a smooth, gradual stall, resulting in more time for stall recovery. A high benefit margin makes SETE an ideal option to achieve more cruise flight efficiency. *This repository contains: <strong>Datasheet </strong> Datasheet Contents: Sheet 1: Wind Tunnel Experiment Data (Paper section <strong>IV.A.3</strong>) Sheet 2: CFD Simulation Data (Paper section <strong>IV.B.3</strong>) Sheet 3: Baseline Model (Paper section <strong>IV.A.1-2</strong>) Sheet 4: Calculation of Lift Increment (Paper section <strong>IV.C</strong>) Sheet 5: Calculation of Benefit Margin (Paper section <strong>IV.D</strong>) Sheet 6: Coefficient of Pressure sample (Paper section <strong>IV.B.3</strong>) <strong>CAD geometries in .STEP format</strong> Ansys Workbench files (Upon request) Contact: [e-mail]论文标题：采用静态延伸尾缘（Static Extended Trailing Edge, SETE）提升气动性能的实验与计算策略 论文摘要：本研究针对加装于NACA0012翼型机翼模型的多款静态延伸尾缘（Static Extended Trailing Edge, SETE）开展开环风洞实验与计算流体动力学（Computational Fluid Dynamics, CFD）仿真，以探究低雷诺数工况下SETE对气动特性的影响。弦长20%、偏转角15°的薄型延伸尾缘，相较于基准模型可提升74.24%的升力。SETE可实现平稳且渐进的失速过程，为失速恢复预留更为充足的时间。较高的效益裕度使SETE成为提升巡航飞行效率的理想方案。 本仓库包含如下内容：<strong>数据集文档</strong> 数据集文档包含以下工作表： 表1：风洞实验数据（对应论文<strong>IV.A.3</strong>章节） 表2：CFD仿真数据（对应论文<strong>IV.B.3</strong>章节） 表3：基准模型数据（对应论文<strong>IV.A.1-2</strong>章节） 表4：升力增量计算数据（对应论文<strong>IV.C</strong>章节） 表5：效益裕度计算数据（对应论文<strong>IV.D</strong>章节） 表6：压力系数示例数据（对应论文<strong>IV.B.3</strong>章节） <strong>.STEP格式的CAD几何模型</strong> Ansys Workbench工程文件（需申请获取） 联系方式：[e-mail]