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Pneumatic Flap Performance for a 2D Circulation Control Airfoil, Steady Pulsed

机译:用于2D循环控制翼型,稳定和脉冲的气动皮瓣性能

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Circulation Control technologies have been around for 65 years, and have been successfully demonstrated in laboratories and flight vehicles alike, yet there are few production aircraft flying today that implement these advances. Circulation Control techniques may have been overlooked due to perceived unfavorable trade offs of mass flow, pitching moment, cruise drag, noise, etc. Improvements in certain aspects of Circulation Control technology are the focus of this paper. This report will describe airfoil and blown high lift concepts that also address cruise drag reduction and reductions in mass flow through the use of pulsed pneumatic blowing on a Coanda surface. Pulsed concepts demonstrate significant reductions in mass flow requirements for Circulation Control, as well as cruise drag concepts that equal or exceed conventional airfoil systems.
机译:循环控制技术已经发生在65年,并已在实验室和飞行车中成功展示,但今天少数生产飞机飞行落实这些进展。由于循环控制技术的某些方面的某些方面,由于感知的不利贸易问题,可能已经被忽略了循环控制技术可能被忽视。循环控制技术的某些方面的改进是本文的焦点。本报告将描述翼型和吹出的高升降​​概念,也通过在坐标表面上使用脉冲气动吹气来解决巡航减少和降低质量流量。脉冲概念表现出对循环控制的质量流量要求的显着降低,以及等于或超过传统翼型系统的巡航阻力概念。

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