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Mitigation of Pusher-Propeller Installation Effects by Pylon Trailing-Edge Blowing

机译:通过塔架后缘吹气来减轻推进器和螺旋桨的安装效果

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摘要

This paper presents an experimental assessment of the working principles of pylon trailing-edge blowing for the mitigation of the interaction between a pusher propeller and its associated pylon. The experiments were performed at the Large Low-Speed Facility of the German-Dutch wind tunnels, using a powered propeller model and an upstream pylon equipped with a trailing-edge blowing system. Inflow microphone measurements demonstrated the impact of pylon installation on the propeller's tonal noise emissions, with increases of up to 16 dB relative to the isolated propeller. Analysis of the unsteady blade pressures showed that this installation effect was caused by the impulsive increase in blade loading during the pylon-wake passage. The efficacy of pylon trailing-edge blowing to reduce the momentum deficit in the pylon wake was confirmed by stereoscopic particle-image-velocimetry measurements between the pylon and the propeller. Consequently, application of the pylon-blowing system alleviated the pylon-installation effects at the source. At an intermediate thrust setting, the rms of the blade-load fluctuations due to the wake encounter was reduced by up to 60%, resulting in noise emissions approximately equal to those recorded for the isolated propeller.
机译:本文提出了对塔架后缘吹气工作原理的实验评估,以减轻推进器螺旋桨及其相关塔架之间的相互作用。实验是在德国-荷兰风洞的大型低速设施中进行的,使用动力推进器模型和配备后缘吹气系统的上游塔架。流入麦克风的测量结果表明,吊塔安装对螺旋桨音调噪声的影响,相对于隔离式螺旋桨而言,增加高达16 dB。对非稳态叶片压力的分析表明,这种安装效果是由塔架/尾流通道期间叶片载荷的脉冲增加引起的。通过在塔架和螺旋桨之间进行立体粒子图像测速仪测量,证实了塔架后缘吹气减少塔架尾流动量不足的功效。因此,塔吊系统的应用从源头上减轻了塔吊的安装效果。在中间推力设置下,由于遭遇尾流而引起的叶片负载波动的均方根值降低了60%,从而导致噪声排放大约等于隔离式螺旋桨记录的噪声排放。

著录项

  • 来源
    《Journal of Aircraft》 |2017年第1期|292-300|共9页
  • 作者单位

    Delft Univ Technol, Fac Aerosp Engn, Flight Performance & Prop Sect, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Fac Aerosp Engn, Aeroacoust Sect, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Fac Aerosp Engn, Flight Performance & Prop Sect, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Fac Aerosp Engn, Flight Performance & Prop Sect, NL-2629 HS Delft, Netherlands;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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