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Parametric Investigation of the Effect of Hub Pitching Moment on Blade Vortex Interaction (BVI) Noise of an Isolated Rotor.

机译：轮毂俯仰力矩对离心转子叶片涡相互作用（BVI）噪声影响的参数研究。

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Malpica, C.; Greenwood, E.; Sim, B.;
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年度 2016
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
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关键词
Blade Vortex Interaction (BVI); Rotocraft;

机译：Blade Vortex Interaction（BVI）; Rotocraft;

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专利

1. Reduction of Blade-Vortex Interaction (BVI) Noise through X-Force Control [J] . Fredric H. Schmitz, Ph. D. Journal of the American Helicopter Society . 1998,第1期

机译：通过X力控制降低叶片-涡旋相互作用（BVI）噪声
2. Localized Individual Blade Root Pitch Control for Helicopter Blade-Vortex Interaction Noise Reduction [J] . Brendon Malovrh, Farhan Gandhi Journal of the American Helicopter Society . 2010,第3期

机译：局部桨叶根桨距控制可降低直升机桨叶-涡流相互作用的噪声
3. Numerical investigation on noise reduction of rotor blade-vortex interaction using blade surface jet blowing [J] . Sun Yan, Xu Guohua, Shi Yongjie Aerospace science and technology . 2021,第Sepa期

机译：叶片表面喷射吹塑转子叶片 - 涡旋相互作用降噪的数值研究
4. Parametric Investigation of the Effect of Hub Pitching Moment on Blade Vortex Interaction (BVI) Noise of an Isolated Rotor [C] . Carlos Malpica, Eric Greenwood, Ben Sim American Helicopter Society International annual forum . 2016

机译：轮毂俯仰力矩对孤立转子叶片涡旋相互作用（BVI）噪声影响的参数研究
5. Non-harmonic root-pitch individual-blade control for the reduction of blade-vortex interaction noise in rotorcraft. [D] . Malovrh, Brendon D. 2013

机译：非谐波根音单个桨叶控制，用于降低旋翼飞机的桨叶-涡流相互作用噪声。
6. Investigation on the Mechanism and Parametric Description of Non-Synchronous Blade Vibration [O] . Mingming Zhang, Anping Hou, Yadong Han 2021

机译：非同步叶片振动机理和参数描述的研究
7. Rotor system having alternating length rotor blades for reducing blade-vortex interaction (BVI) noise [O] . Moffitt, Robert C., Visintainer, Joseph A. 1997

机译：具有交替长度的转子叶片的转子系统，用于减少叶片涡流相互作用（BVI）噪声
8. Parametric Investigation of the Effect of Hub Pitching Moment on Blade Vortex Interaction (BVI) Noise of an Isolated Rotor. [R] . Malpica, C., Greenwood, E., Sim, B. 2016

机译：轮毂俯仰力矩对离心转子叶片涡相互作用（BVI）噪声影响的参数研究。

Parametric Investigation of the Effect of Hub Pitching Moment on Blade Vortex Interaction (BVI) Noise of an Isolated Rotor.

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