从总体设计角度透视高超声速飞行器边界层转捩问题

李志文; 袁海涛; 黄斌; 张增辉; 于新源

doi:10.7638/kqdlxxb-2020.0061

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从总体设计角度透视高超声速飞行器边界层转捩问题

综述 | 更新时间：2026-05-28

- 从总体设计角度透视高超声速飞行器边界层转捩问题
- The hypersonic boundary-layer transition: a perspective from the view of system design
- 空气动力学学报 2021年39卷第4期页码：26-38
- 作者机构：
  
  北京机电工程总体设计部,北京,100854
- 作者简介：
  
  李志文*（1978-），男，湖南永顺人，研究员，研究方向：飞行器总体设计. E-mail：66473583@qq.com
- 基金信息：
- DOI：10.7638/kqdlxxb-2020.0061
  中图分类号： O357.4+1
- 纸质出版：2021
- 稿件说明：
移动端阅览
李志文, 袁海涛, 黄斌, 等. 从总体设计角度透视高超声速飞行器边界层转捩问题[J]. 空气动力学学报, 2021, 39(4): 26−38.

LI Zhiwen, YUAN Haitao, HUANG Bin, et al. The hypersonic boundary-layer transition: a perspective from the view of system design[J]. 2021, 39(4): 26-38.
李志文, 袁海涛, 黄斌, 等. 从总体设计角度透视高超声速飞行器边界层转捩问题[J]. 空气动力学学报, 2021, 39(4): 26−38. DOI： 10.7638/kqdlxxb-2020.0061

LI Zhiwen, YUAN Haitao, HUANG Bin, et al. The hypersonic boundary-layer transition: a perspective from the view of system design[J]. 2021, 39(4): 26-38. DOI： 10.7638/kqdlxxb-2020.0061.

摘要

边界层转捩对飞行器总体性能影响很大，按照弹道式再入、再入机动、高超声速滑翔、高超声速巡航四类飞行器进行分类，与边界层转捩相关的典型问题可归结为气动力、气动热及掺混效率三类，相应带来飞行稳定性与配平能力、落点散布、防热风险、飞行器减重、推进系统优化等问题。针对边界层转捩控制问题，从总体设计方面可采取弹道设计、翼载荷控制、外形设计、材料选择等措施，推迟或诱发转捩，以达到减阻、减热、掺混等设计目标。总体设计单位应重视开展静音风洞试验，充分利用飞行任务资源积累转捩研究基础数据，努力提高理论分析与预示能力，牵引开发高效、高精度的转捩分析工具。

Abstract

The boundary-layer transition (BLT) has a great impact on the performance of hypersonic vehicles. Typical BLT problems are reviewed concerning hypersonic vehicles with four different types of trajectories known as ballistic reentry

maneuverable reentry

hypersonic glide

and hypersonic cruise. Relating issues are discussed including dynamic stability

trim

impact point dispersion

thermal protection

vehicle weight reduction

and propulsion system optimization

etc.

all of which can be attributed to aerodynamic force

aeroheating

and mixing efficiency that BLT impacts directly. Potential methods are suggested to control BLT for system design including adjustments of trajectory

wing load

and aerodynamic configuration

and selection of proper materials

etc.

for drag reduction

aeroheating alleviation

and mixing efficiency enhancement. It is beneficial for system-design institutes to utilize quiet wind-tunnel and flight tests to acquire more experience and knowledge about BLT. Efforts should be made to enhance the capability of developing efficient and precise theoretical analyses and prediction tools.

关键词

Keywords

references

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