高超声速飞行器机体/推进一体化设计的启示

doi:10.7527/S1000-6893.2014.0226

总体气动与综合

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高超声速飞行器机体/推进一体化设计的启示

罗金玲¹, 李超¹, 徐锦²

1. 北京空天技术研究所, 北京 100074;
2. 北京机电工程研究所, 北京 100074

收稿日期:2014-06-11 修回日期:2014-10-08 出版日期:2015-01-15 发布日期:2015-01-24
通讯作者: 罗金玲,Tel.: 010-68191238 E-mail: 13601293188@139.com E-mail:13601293188@139.com
作者简介:罗金玲女, 博士, 研究员。主要研究方向: 飞行器设计。 Tel: 010-68191238 E-mail: 13601293188@139.com
基金资助:
国家级项目

Inspiration of hypersonic vehicle with airframe/propulsion integrated design

LUO Jinling¹, LI Chao¹, XU Jin²

1. Beijing Aerospace Technology Institute, Beijing 100074, China;
2. Beijing Electro-Mechanical Engineering Institute, Beijing 100074, China

Received:2014-06-11 Revised:2014-10-08 Online:2015-01-15 Published:2015-01-24
Supported by:
National Level Project

摘要/Abstract

摘要：

机体/推进一体化设计是吸气式高超声速飞行器的关键技术。飞行器的前体和后体既是主要的气动型面,又是发动机进气道的外压缩型面和尾喷管的膨胀型面,一体化设计直接影响飞行器的气动与发动机性能。本文阐述了吸气式高超声速飞行器的主要特点,梳理了飞行器的推阻匹配、升阻比特性、操稳匹配等主要气动设计问题。通过对国外典型高超声速飞行器机体/推进一体化设计技术的综合分析,总结了前体/进气道、后体/尾喷管、边界层强制转捩装置等关键部件的气动设计方法,获得了有意义的启示,可为后续吸气式高超声速技术研究提供重要参考。

关键词: 高超声速飞行器, 机体/推进一体化设计, 前体/进气道, 后体/尾喷管, 强制转捩装置

Abstract:

Airframe/propulsion integrated design is the key technology for hypersonic vehicles. The fore-body and the after-body of vehicles are not only aerodynamic surface, but also either the external-compression surface of engine inlet or the expansion surface of rear nozzle. Hence airframe/propulsion integrated design directly affects aerodynamic characteristics and performances of propulsion. In this paper, the main characteristics of hypersonic vehicle is introduced and crucial aerodynamics issues such as thrust matching with drag and lift-to-drag ratio, as well as maneuverability matching with stability etc., are reviewed. Through a comprehensive analysis of airframe/propulsion integrated design techniques, based on foreign typical hypersonic vehicles and aerodynamic design methods of critical components, the fore-body/inlet integration, after-body/nozzle integration and forced boundary-layer transition device etc., are summarized and some valuable inspirations are obtained. The conclusions could provide important references for the investigation of air-breathing hypersonic technology.

Key words: hypersonic vehicle, airframe/propulsion integrated design, fore-body/inlet, after-body/nozzle, forced transition device

中图分类号:

罗金玲, 李超, 徐锦. 高超声速飞行器机体/推进一体化设计的启示[J]. 航空学报, 2015, 36(1): 39-48.

LUO Jinling, LI Chao, XU Jin. Inspiration of hypersonic vehicle with airframe/propulsion integrated design[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 39-48.

参考文献

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E-mail：hkxb@buaa.edu.cn

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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

高超声速飞行器机体/推进一体化设计的启示

Inspiration of hypersonic vehicle with airframe/propulsion integrated design

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