无尾布局后体超声速航向增稳设计方法

doi:10.7527/S1000-6893.2019.23447

流体力学与飞行力学

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

无尾布局后体超声速航向增稳设计方法

李春鹏, 刘铁中, 钱战森, 张铁军

中国航空工业空气动力研究院, 高速高雷诺数气动力航空科技重点实验室, 沈阳 110034

收稿日期:2019-09-04 修回日期:2019-10-21 出版日期:2020-06-15 发布日期:2019-11-07
通讯作者: 李春鹏 E-mail:xincewei@163.com
基金资助:
装备预研共用技术项目（41406030301）

After body supersonic directional stability augmentation method for tailless configuration

LI Chunpeng, LIU Tiezhong, QIAN Zhansen, ZHANG Tiejun

Aero Science Key Lab of High Reynolds Aerodynamic Force at High Speed, AVIC Aerodynamics Research Institute, Shenyang 110034, China

Received:2019-09-04 Revised:2019-10-21 Online:2020-06-15 Published:2019-11-07
Supported by:
Common Technology Project of Equipment Development Department(41406030301)

摘要/Abstract

摘要： 针对无尾布局超声速航向静稳定性不足的问题，提出一种基于超声速压缩/膨胀流动的后体超声速航向气动增稳设计方法。首先通过无尾布局扁平后体和常规后体方案航向静稳定性和表面流场差异的对比，明确了后体超声速航向增稳设计思路。然后基于后体参数化外形分析了后体型面对于布局超声速航向静稳定性的影响规律。最后通过评估典型后体方案的综合气动特性验证了后体超声速航向增稳设计方法的可行性。研究表明：重心后侧向投影面积增量、后体脊线以及后体截面曲线是影响后体型面超声速航向增稳能力的3个主要参数。与常规后体型面相比，通过超声速航向增稳设计获得的后体型面能够在布局阻力变化不大的情况下，显著改善无尾布局在跨声速和超声速状态的航向静不稳定性。

关键词: 无尾布局, 后体, 超声速, 航向静稳定性, 气动增稳

Abstract: Aiming at the problem of insufficient supersonic directional static stability in the tailless configuration aircraft design, an aerodynamic supersonic directional augmentation method for the after-body design is presented. Firstly, the design idea of after-body supersonic directional augmentation was made clear by the comparative analysis of the directional static stability and surface flow field between flat after-body and conventional after-body of tailless configuration. And then the influence law of the after-body shape on the supersonic directional static stability was analyzed based on the parametric configuration. Finally, the effectiveness of the after body supersonic directional stability augmentation method was verified by the comprehensive aerodynamic characteristics numerical evaluation of the typical after-body scheme. The results show that the increment of after-body lateral projected area, after-body surface spine curves and after-body surface section curves are the three most important parameters which affect the ability of after body supersonic directional augmentation. Compared to the conventional after-body, the after-body shape designed by the supersonic directional augmentation method can dramatically decrease the directional static instability of the tailless configuration at transonic and supersonic flight with drag basically unchanged.

Key words: tailless configuration, after body, supersonic, directional static stability, aerodynamic stability augmentation

中图分类号:

V211.3

李春鹏, 刘铁中, 钱战森, 张铁军. 无尾布局后体超声速航向增稳设计方法[J]. 航空学报, 2020, 41(6): 523447-523447.

LI Chunpeng, LIU Tiezhong, QIAN Zhansen, ZHANG Tiejun. After body supersonic directional stability augmentation method for tailless configuration[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(6): 523447-523447.

参考文献 21

[1]	车竞, 何开锋, 钱炜祺. 制空型无人机的关键技术、气动布局及特性[J]. 空气动力学学报, 2017, 35(1):13-26. CHE J, HE K F, QIAN W Q. Key technique and aerodynamic configuration characteristic of UCAV with command of the air[J]. Acta Aerodynamica Sinica, 2017, 35(1):13-26(in Chinese).
[2]	孙隆和. 第六代战斗机的竞争[J]. 电光与控制, 2012, 19(10):1-7. SUN L H. The competition of the sixth generation fighters[J]. Electronics Optics and Control, 2012, 19(10):1-7(in Chinese).
[3]	石怀林, 武卫兵, 张立, 等. 美军第六代战斗机典型技术特征[J]. 国防科技, 2010, 31(4):10-13. SHI H L, WU W B, ZHANG L, et al. A review on the typical technic characters of fighters of the sixth generation in the U.S. air force[J]. National Defense Science and Technology, 2010, 31(4):10-13(in Chinese).
[4]	李金梁, 涂泽中, 刘振庭. 美第六代战斗机研究进展情况[J]. 电光与控制, 2014, 21(6):3-8. LI J L, TU Z Z, LIU Z T. The research progress of the sixth generation fighter of USAF[J]. Electronics Optics and Control, 2014, 21(6):3-8(in Chinese).
[5]	SATHE A, PANT R. Conceptual design studies of an unmanned combat aerial vehicle:AIAA-2010-9306[R]. Reston:AIAA, 2010.
[6]	ADDINGTON G A, MYATT J H. Control surface deflection effects on the innovative control effectors (ICE 101) design:AFRL-VA-WP-T R-2000-3027[R]. Reston:AFRL, 2010.
[7]	BOWLUS J A, MULTHOPP D, BANDA S S. Challenges and opportunities in tailless aircraft stability and control:AIAA-1997-3830[R]. Reston:AIAA, 1997.
[8]	DORSETT K M, MEHL D R. Innovative control effectors(ICE):WL-TR-96-3043[R]. Reston:AFRL, 1996.
[9]	马松辉, 吴成富, 陈怀民. 飞翼飞机稳定性与操纵性研究[J]. 飞行力学, 2006, 24(3):17-21. MA S H, WU C F, CHEN H M. Study on stability and maneuverability of flying wing aircraft[J]. Flight Dynamics, 2006, 24(3):17-21(in Chinese).
[10]	GILLARD W J, DORSETT K M. Directional control for tailless aircraft using all moving tips:AIAA-1997-3487[R]. Reston:AIAA, 1997.
[11]	李忠剑, 马东立. 飞翼布局阻力类偏航操纵装置操纵特性分析[J]. 北京航空航天大学学报, 2014, 40(5):695-700. LI Z J, MA D L. Control characteristics analysis of drag yawing control devices of flying wing configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5):695-700(in Chinese).
[12]	张彬乾, 马怡, 褚胡冰, 等. 小展弦比飞翼布局航向控制的组合舵面研究[J]. 航空学报, 2013, 11(34):2436-2443. ZHANG B Q, MA Y, CHU H B, et al. Investigation on combined control surfaces for the yaw control of low aspect ratio flying wing configuration[J]. Acta Aeronautica et Astronautica Sinica, 2013, 11(34):2436-2443(in Chinese).
[13]	单继祥, 黄勇, 苏继川, 等. 小展弦比飞翼布局新型嵌入面航向控制特性研究[J]. 空气动力学学报, 2015, 33(3):296-301. SHAN J X, HUANG Y, SU J C, et al. Effect of the novel embedded control surfaces on direction control characteristic of low-aspect-ratio flying-wing configuration[J]. Acta Aerodynamica Sinica, 2015, 33(3):296-301(in Chinese).
[14]	BOLSUNOVSKY A L, BUZOVERYA N P, GUREVICH B I, et al. Flying wing problems and decisions[J]. Aircraft Design, 2001, 4:193-219.
[15]	DMITRIEV V G, DENISOV V E, GUREVICH B I, et al. The flying wing concept chances and risks:AIAA-2003-2887[R]. Reston:AIAA, 2003.
[16]	ESTENBAN S. Static and dynamic analysis of an unconventional plane flying wing:AIAA-2001-4010[R]. Reston:AIAA, 2001.
[17]	冯立好, 王晋军, 于东升. 多操纵面无尾布局飞机横航向控制[J]. 北京航空航天大学学报, 2010, 36(9):1038-1042. FENG L H, WANG J J, YU D S. Lateral-directional control of tailless aircraft with multiple control surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(9):1038-1042(in Chinese).
[18]	李林, 马超, 王立新. 小展弦比飞翼布局飞机稳定特性[J]. 航空学报, 2007, 28(6):1312-1317. LI L, MA C, WANG L X. Stability features of low aspect-ratio flying wings[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(6):1312-1317(in Chinese).
[19]	STENFELT G, RINGERTZ U. Yaw control of a tailless aircraft configuration[J]. Journal of Aircraft, 2010, 47(5):1807-1810.
[20]	宋磊, 杨华, 颜旭峰, 等. 飞翼无增稳条件下横航向动稳定设计方法[J]. 系统工程与电子技术, 2015, 37(11):2561-2565. SONG L, YANG H, YAN X F, et al. Increasing the flying wing lateral-directional dynamic stability without relying on augmentation system[J]. Systems Engineering and Electronics, 2015, 37(11):2561-2565(in Chinese).
[21]	赵俊波, 沈清. 升力体布局飞行器偏航气动增稳方法研究[J]. 空气动力学学报, 2016, 34(3):322-326. ZHAO J B, SHEN Q. Directional stability augmentation method for a lifting body configuration[J]. Acta Aerodynamica Sinica, 2016, 34(3):322-326(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

无尾布局后体超声速航向增稳设计方法

After body supersonic directional stability augmentation method for tailless configuration

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献 21

相关文章 15

编辑推荐

Metrics

本文评价

[1]	乔竑玮, 梁剑寒, 张林, 孙明波, 陈玉俏. 超声速燃烧中的概率密度函数方法研究进展[J]. 航空学报, 2024, 45(8): 28802-028802.
[2]	郑建成, 曲智国, 谭贤四, 李志淮, 朱刚, 李陆军, 刘伟. 基于责任区划分的雷达网探测高超声速目标资源管理[J]. 航空学报, 2024, 45(8): 329022-329022.
[3]	戴今钊, 陈海昕. 流场波系引导的三维消波翼优化设计方法[J]. 航空学报, 2024, 45(6): 628942-628942.
[4]	李军府, 陈晴, 王伟, 韩忠华, 谭玉婷, 丁玉临, 谢露, 乔建领, 宋科, 艾俊强. 一种先进超声速民机低声爆高效气动布局设计[J]. 航空学报, 2024, 45(6): 629613-629613.
[5]	刘小勇, 王明福, 刘建文, 任鑫, 张轩. 超燃冲压发动机研究回顾与展望[J]. 航空学报, 2024, 45(5): 529878-529878.
[6]	杨博, 于贺, 樊子辰. 微观能量分析气动光学效应时变误差的方法[J]. 航空学报, 2024, 45(4): 128703-128703.
[7]	纪鉴恒, 蔡尊, 王泰宇, 孙明波, 王振国. 宽速域超燃冲压发动机流动燃烧过程研究进展[J]. 航空学报, 2024, 45(3): 28696-028696.
[8]	赖江, 范召林, 王乾, 董思卫, 童福林, 袁先旭. 高超声速有攻角锥裙直接数值模拟[J]. 航空学报, 2024, 45(2): 128610-128610.
[9]	李学良, 李创创, 苏伟, 吴杰. 分布式粗糙元对高超声速边界层不稳定性的影响试验[J]. 航空学报, 2024, 45(2): 128627-128627.
[10]	王一凡, 陈浩颖, 张海波. 面向巡航任务的自适应循环发动机进/发匹配[J]. 航空学报, 2024, 45(2): 128637-128637.
[11]	熊有德, 李创创, 张振辉, 吴杰. 高超声速风洞自由来流扰动热线测量技术[J]. 航空学报, 2024, 45(10): 129042-129042.
[12]	倪炜霖, 王永海, 徐聪, 赤丰华, 梁海朝. 基于强化学习的高超飞行器协同博弈制导方法[J]. 航空学报, 2023, 44(S2): 729400-729400.
[13]	于哲峰, 梁世昌, 石卫波, 田得阳, 石安华, 廖东骏, 杨鹰. 类HTV⁃2飞行器光电特性的分析评估技术[J]. 航空学报, 2023, 44(S2): 729465-729465.
[14]	马平, 张宁, 石安华, 于哲峰, 梁世昌, 黄洁. 典型微波波段信号在模拟等离子体中的传输特性[J]. 航空学报, 2023, 44(S2): 729476-729476.
[15]	陈浩宇, 王彬文, 宋巧治, 李晓东. 热颤振地面模拟试验技术[J]. 航空学报, 2023, 44(8): 227295-227295.