【航宇大讲堂】Study on two-element high lift airfoil for long endurance flight at low Reynolds numbers

作者:时间:2019-10-18浏览:354供图:审阅:来源:乐投Letou

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报告题目:Study on two-element high lift airfoil for long endurance flight at low Reynolds numbers

报告人:Dr. Y D CUI (Temasek Laboratories, National University of Singapore)

报告时间:20191021日(周一)14:30

报告所在:明故宫校区C12-619

主办单位:航空学院,非定?掌ρв肓鞫刂乒ば挪恐氐闶笛槭

报告内容简介:

Conventional high lift devices of airplane are of a compromise design between the requirements of optimal cruising and taking-off/landing conditions. The study on the high lift system’s aerodynamics remains in the forefront of research to achieve more efficient flight. In recent years, unmanned aerial vehicles (UAVs) have been extensively studied and developed. Unlike commercial airplanes to pursue long range and speed, some UAVs usually look for long endurance for surveillance purpose. This requirement provides a chance for a two-element high lift airfoil being used for UAVs to achieve a longer endurance factor. In this talk, some of our preliminary studies on two-element airfoil design with wind tunnel test and numerical simulations will be presented and discussed.   

 

报告人简介:

Dr. Cui is a Senior Research Scientist at Temasek Laboratories and a Teaching Associate at the Department of Mechanical Engineering of the National University of Singapore. He obtained his BEng and MEng from Nanjing University of Aeronautics and Astronautics, China, and PhD from NUS. His research interests include flow visualization and experimental techniques, vortex flow, high lift devices, drag reduction, and flow control. He is a senior member of the American Institute of Aeronautics and Astronautics (AIAA).      


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