Design parameters improvement of helicopter ducted tail rotor

Zhong Guo; Huang Jun; Yi Mingxu

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Design parameters improvement of helicopter ducted tail rotor

机译：直升机风管尾桨设计参数的改进

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摘要

Purpose The purpose of this paper is to reduce the acoustic noise of helicopter ducted tail rotor.

机译：目的本文的目的是减少直升机导管式尾桨的噪声。

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来源
《Aircraft engineering》 |2018年第2期|237-245|共9页
作者
Zhong Guo; Huang Jun; Yi Mingxu;
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作者单位

Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China;

Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China;

Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China;

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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
Aerodynamic noise; Computational fluid dynamics; Ducted tail rotor; Noise reduction;

机译：空气动力学噪声;计算流体力学;尾翼转子;降噪;

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专利

1. Characterization and Selection of Basic Parameters for Steering Servo of a Small Remotely-Piloted Single-Rotor Helicopter with Tail Rotor [J] . D. A. Dyakonov, O. A. Zavalov, D. A. Kuptsov, Russian Aeronautics . 2014,第4期

机译：小型尾翼小型遥控单旋翼直升机转向伺服基本参数的表征与选择
2. DESIGN OF FLY-BY-WIRE CONTROL SYSTEM ALGORITHMS FOR SINGLE-ROTOR HELICOPTER WITH TAIL ROTOR AT HOVERING MODE [J] . Vladimir Mikhailovich Kuvshinov, Veniamin Aleksandrovich Leontiev TsAGI science journal . 2019,第3期

机译：尾模单桨直升机悬停飞行时线控系统算法设计
3. Aerodynamic Characteristics of Helicopter with Ducted Fan Tail Rotor in Hover under Low-Speed Crosswind [J] . Nahyeon Roh, Sejong Oh, Donghun Park International journal of aerospace engineering . 2020,第4期

机译：低速交流下悬停悬停中带有管道风机尾桨直升机的空气动力学特性
4. Investigation on Loss of Tail-rotor Effectiveness of Helicopter with Ducted Fan Tail Rotor [C] . Nahyeon Roh, Donghun Park, Sejong Oh European rotorcraft forum . 2018

机译：风管式尾桨直升机的尾桨效能损失研究
5. High-frequency directional axis dynamics of helicopters with ducted tail rotors. [D] . Kothmann, Bruce David. 2000

机译：带导管尾桨的直升机的高频方向轴动力学。
6. Rational improvement of gp41-targeting HIV-1 fusion inhibitors: an innovatively designed Ile-Asp-Leu tail with alternative conformations [O] . Yun Zhu, Shan Su, Lili Qin, -1

机译：合理靶向gp41的HIV-1融合抑制剂：创新设计的Ile-Asp-Leu尾巴具有其他构象
7. Variable-speed tail rotors for helicopters with variable-speed main rotors [O] . Han D., Barakos G.N. 2017

机译：用于带有变速主转子的直升机的变速尾部转子

Design parameters improvement of helicopter ducted tail rotor

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