振荡射流控制方法在无舵面飞行控制中的应用

仇梓豪; 李子焱; 周楷文; 王士奇; 刘应征; 温新

doi:10.11729/syltlx20230045

振荡射流控制方法在无舵面飞行控制中的应用

doi: 10.11729/syltlx20230045

仇梓豪^{1, 2,},
李子焱³,
周楷文¹,
王士奇⁴,
刘应征¹,
温新^1, ,

1.
上海交通大学机械与动力工程学院，上海　200240
2.
中国空气动力研究与发展中心低速空气动力研究所，绵阳　621000
3.
中国船舶科学研究中心水动力学科研部，无锡　214082
4.
中国航空发动机集团中国航空发动机研究院，北京　101304

基金项目: 国家自然科学基金项目（12072196）

详细信息

作者简介:
仇梓豪：（1998—），男，江苏徐州人，硕士研究生。研究方向：实验流体力学，流动控制。通信地址：上海市闵行区东川路800号上海交通大学闵行校区机械与动力工程学院叶轮机械研究所（200240）。E-mail：qiuzihao1117@sjtu.edu.cn

通讯作者:
E-mail：wenxin84@sjtu.edu.cn

中图分类号: V211.7
计量
- 文章访问数: 129
- HTML全文浏览量: 38
- PDF下载量: 28
- 被引次数: 0
出版历程
- 收稿日期: 2023-03-28
- 修回日期: 2023-06-08
- 录用日期: 2023-07-03
- 刊出日期: 2023-08-30

Sweeping jet control mechanism and its application in flapless flight control

QIU Zihao^{1, 2
,},
LI Ziyan³,
ZHOU Kaiwen¹,
WANG Shiqi⁴,
LIU Yingzheng¹,
WEN Xin^{1
, ,}

1.
School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai　200240, China
2.
Low Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang　621000, China
3.
State Key Laboratory of Hydrodynamics, China Ship Scientific Research Center, Wuxi　214082, China
4.
Aero Engine Academy of China, Aero Engine Corporation of China, Beijing　101304, China

摘要

摘要: 利用射流主动流动控制方法，飞行器无舵面飞行控制技术取消了传统的机械舵面，具有附加重量小、控制性能优异等优点，适合隐形设计。本文针对现有定常射流控制方法控制效率较低、耗气量大等问题，介绍了振荡射流在无舵面飞行控制中的应用，概述了2项无舵面飞行控制技术——环量控制技术和流体推力矢量技术——的研究现状，讨论了振荡射流在扩大控制区域、增强掺混和频率调节方面的机理和优势。从环量控制和流体推力矢量2个角度出发，详细介绍了振荡射流在无舵面飞行控制中的应用机理和优异表现。
- 环量控制 /
- 推力矢量 /
- 振荡射流 /
- 流体振荡器 /
- 主动流动控制
Abstract: The flapless aerodynamic control technology of aircraft has the advantages of low additional weight, excellent control performance and suitability for stealth design by using the active flow control method of jets and eliminating the traditional mechanical flap surface. This paper presents the application of sweeping jets in flapless aerodynamic layouts to address the problem of high air consumption caused by the low control efficiency of existing steady jet control methods. This paper outlines the current research status of two flapless control technologies, i.e., circulation control and fluidic thrust vectoring, and then discusses the mechanism and advantages of the sweeping jet in terms of control area, enhanced flow mixing, and frequency regulation. The mechanism and performance of the sweeping jet in flapless flight control are presented in detail in terms of circulation control and thrust vectoring.
- circulation control /
- thrust vectoring /
- sweeping jet /
- fluidic oscillator /
- active flow control

HTML全文

图 1 环量控制翼型示意图

Figure 1. Schematic of a wing using circulation control

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图 2 同向二次流控制方法原理示意图

Figure 2. The schematic diagram of the principle of the co-directional secondary flow control method

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图 3 双反馈通道流体振荡器原理示意图

Figure 3. Schematic of a fluidic oscillator with two feedback channels

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图 4 毫米级流体振荡器

Figure 4. Millimeter-scale fluid oscillator

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图 5 Jones等的环量控制翼型几何设计^[54]

Figure 5. Geometric details of the circulation control wings from Jones^[54]

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图 6 SACCON模型配置示意图^[55]

Figure 6. Schematic of the configuration in SACCON^[55]

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图 7 Li等的环量控制翼型几何设计^[56]

Figure 7. Geometric details of the circulation control wings from Li^[56]

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图 8 不同射流驱动下环量控制翼型的气动特性

Figure 8. Aerodynamic characteristics of different jet driven circulation control wings

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图 9 Wen等的实验装置设计^[52]

Figure 9. Schematic of the experimental device design from Wen^[52]

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图 10 二次流控制下的主射流偏转情况

Figure 10. The main jet deflection under secondary flow control

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