Drag Reduction Of A Swept Wing By Means Of Plasma Actuators

Sergey Chernyshev,Marat Gamirullin,Andrey Kiselev,Aleksandr Kuryachii, Sergey Manuilovich, Dmitry Sboev

IRF2018: PROCEEDINGS OF THE 6TH INTERNATIONAL CONFERENCE ON INTEGRITY-RELIABILITY-FAILURE（2018）

引用 0|浏览0

暂无评分

摘要

This work presents some recent results of theoretical and experimental study of innovative laminar flow control method on a swept wing based on electrogasdynamic impact on boundary layer flow. Experimental verification of this method is supposed to be carried out in near future in low-turbulence subsonic wind tunnel with the use of new multi-discharge plasma actuator system.

查看译文

关键词

swept wing, laminar-to-turbulent transition, dielectric barrier discharge actuator

AI 理解论文

溯源树

样例

生成溯源树，研究论文发展脉络

Chat Paper

正在生成论文摘要