Helicopter stabilizer optimization considering rotor downwash in forward-flight

Minervino Mauro; Vitagliano Pier Luigi; Quagliarella Domenico

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Helicopter stabilizer optimization considering rotor downwash in forward-flight

机译：考虑前向飞行中的转子向下冲洗的直升机稳定器优化

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摘要

Purpose - The paper aims to reduce the aerodynamic drag of a rotorcraft stabilizer in forward flight by taking into account downwash effects from the main rotor wake (power-on conditions).

机译：目的-本文旨在通过考虑主旋翼尾流（通电条件）产生的下冲作用来减少旋翼飞行器稳定器在向前飞行中的空气阻力。

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来源
《Aircraft engineering and aerospace technology》 |2016年第6期|846-865|共20页
作者
Minervino Mauro; Vitagliano Pier Luigi; Quagliarella Domenico;
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作者单位

CIRA SCpA, Italian Aerosp Res Ctr, Dept Fluid Mech, Capua, CE, Italy;

CIRA SCpA, Italian Aerosp Res Ctr, Dept Fluid Mech, Capua, CE, Italy;

CIRA SCpA, Italian Aerosp Res Ctr, Dept Fluid Mech, Capua, CE, Italy;

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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
Optimization; Helicopter; CFD; CAD-in-the-loop; Forward flight; RotorCraft;

机译：优化;直升机;CFD;在环CAD;前向飞行;转子工艺;

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1. Downwash distribution of single-rotor unmanned agricultural helicopter on hovering state [J] . Songchao Zhang, Xinyu Xue, Zhu Sun, International Journal of Agricultural and Biological Engineering . 2017,第5期

机译：悬停状态下单旋翼无人农业直升机的下冲分布
2. Effects of rotor downwash on exhaust plume flow and helicopter infrared signature [J] . Cheng-xiong Pan, Jing-zhou Zhang, Li-feng Ren, Applied thermal engineering: Design, processes, equipment, economics . 2014,第1a2期

机译：旋翼下冲对排气羽流和直升机红外信号的影响
3. Performance Optimization of Forward-Flight and Lift-Up Phases in a Cycloidal Rotor Using an Active Control Mechanism [J] . Habibnia Rami Mehdi, Pascoa Jose Carlos Journal of aerospace engineering . 2021,第4期

机译：使用主动控制机制在摆线转子中的正向和升降阶段的性能优化
4. Stabilization of unmanned helicopter with suspended payload in presence of wind gusts and rotor downwash [C] . Hassaan Afzal, Fahad Mumtaz Malik International Conference on Electrical and Electronic Engineering . 2018

机译：在阵风和旋翼下冲的情况下稳定具有悬浮有效载荷的无人直升机
5. DYNAMICS OF A HELICOPTER WITH A SLING LOAD (ROTOR DOWNWASH, MILVAN, UNSTEADY AERODYNAMICS, CH-53, TRIM). [D] . RONEN, TUVYA. 1986

机译：带有吊索载荷的直升机的动力学特性（转子下降，米尔文，不稳定气动，CH-53，TRIM）。
6. Post-movement stabilization time for the downwash region of a 6-rotor UAV for remote gas monitoring [O] . Jacob L. Brinkman, Brent Davis, Catherine E. Johnson 2020

机译：用于远程气体监测的6转子UAV的后移动后稳定时间
7. Downwash distribution of single-rotor unmanned agricultural helicopter on hovering state [O] . Zhang Songchao, Xue Xinyu, Sun Zhu, 2017

机译：单圈无人农业直升机在悬停状态下的灌水分布
8. THE EFFECT OF FORWARD-FLIGHT SPEED ON THE PROPULSIVE CHARACTERISTICS OF A PULSE-JET ENGINE MOUNTED ON A HELICOPTER ROTOR [R] . Robert D. Powell 1957

机译：前飞速对直升机转子上脉冲发动机推进特性的影响

Helicopter stabilizer optimization considering rotor downwash in forward-flight

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