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高速空气舵横-逆向双射流耦合流动控制及降热特性

骆俊衡 郭庆阳 王林 刘冰 李世斌

航空学报2026,Vol.47Issue(13):108-126,19.
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航空学报2026,Vol.47Issue(13):108-126,19.DOI:10.7527/S1000-6893.2026.33348

高速空气舵横-逆向双射流耦合流动控制及降热特性

Coupled flow control and heat reduction characteristics of transverse-opposing dual-jets for high-speed air rudder

骆俊衡 1郭庆阳 1王林 1刘冰 1李世斌1

作者信息

  • 1. 国防科技大学 先进推进技术实验室,长沙 410073
  • 折叠

摘要

Abstract

The multi-scale flow coupling effects induced by Shock Wave/Boundary Layer Interaction(SWBLI)in hy-personic flows significantly exacerbate the challenges of thermal load management for flight vehicles.A transverse-opposing dual-jet active control scheme for air rudder is proposed,and its impact characteristics on SWBLI and aero-thermal environments under complex inflow conditions is revealed.The numerical methods employed are validated against experimental data from open literature,and a grid independence analysis is conducted.Results indicate that the transverse-opposing dual-jet scheme achieves global heat reduction superior to single-jet configurations through spatially coupled configurations.Under the condition of an 11° rudder deflection,positioning the transverse jet further upstream and the opposing jet at a higher elevation constructs a large-scale separation zone that isolates the high-temperature mainstream.Consequently,the peak heat fluxes on the leading edge and the plate are controlled below 3 200 kW·m-2 and 300 kW·m-2,respectively.At an angle of attack of 11°,all dual-jet configurations significantly re-duce the gap heat flux to below 300 kW·m-2.However,the leading-edge heat flux is sensitive to jet positioning;it is crucial to ensure the opposing jet remains within the low-pressure wake of the transverse jet to prevent severe flow re-attachment and a subsequent surge in heat flux.

关键词

激波/边界层干扰/空气舵/横-逆向射流/主动流动控制/气动热环境

Key words

shock wave/boundary layer interaction/air rudder/transverse-opposing jets/active flow control/aero-thermal environment

分类

航空航天

引用本文复制引用

骆俊衡,郭庆阳,王林,刘冰,李世斌..高速空气舵横-逆向双射流耦合流动控制及降热特性[J].航空学报,2026,47(13):108-126,19.

基金项目

国家自然科学基金(12372272) (12372272)

国防科技大学自主科研基金(24-ZZCX-XXX-31) National Natural Science Foundation of China(12372272) (24-ZZCX-XXX-31)

Innovation Research Foundation of National University of Defense Technology(24-ZZCX-XXX-31) (24-ZZCX-XXX-31)

航空学报

1000-6893

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