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边界层吸入式进气道气动设计及流动控制技术研究进展

刘雷 张钊睿 汪昆 王志豪 朱晨 谭慧俊 黄河峡

航空学报2026,Vol.47Issue(7):1-33,33.
航空学报2026,Vol.47Issue(7):1-33,33.DOI:10.7527/S1000-6893.2025.32973

边界层吸入式进气道气动设计及流动控制技术研究进展

Research progress on aerodynamic design and flow control technologies for boundary layer ingestion inlets

刘雷 1张钊睿 1汪昆 2王志豪 1朱晨 1谭慧俊 1黄河峡1

作者信息

  • 1. 南京航空航天大学 能源与动力学院,南京 210016
  • 2. 深圳技术大学 城市交通与物流学院,深圳 518118
  • 折叠

摘要

Abstract

Boundary-Layer-Ingesting(BLI)propulsion technology uses a rear mounted engine to draw in the bound-ary layer on the fuselage,reducing the airflow velocity at the inlet of the intake duct and the outlet of the propulsion system,thereby achieving efficient flight of the aircraft.Compared to traditional propulsion systems,BLI propulsion systems have the potential to significantly reduce fuel consumption,flight resistance,and pollution emissions,and are a key development direction in the field of aircraft and engine integration in the future.As a specific practitioner of boundary layer ingesting,the performance of the BLI inlet directly affects the comprehensive benefits of the entire BLI propulsion system compared to traditional propulsion systems.Since its emergence,it has attracted widespread atten-tion from scholars and research institutions at home and abroad.Based on this,this article provides an overview of the research background and progress of BLI intake duct technology,with a focus on discussing the aerodynamic design methods,research methods,internal flow mechanism,and internal flow control technology of BLI intake ducts.Fi-nally,based on the analysis and summary of the current research status at home and abroad,the future development of BLI intake duct is discussed.

关键词

边界层吸入式推进技术/BLI进气道/气动设计/内流机理/内流控制技术

Key words

boundary-layer-ingesting propulsion technology/BLI inlet/aerodynamic design/internal flow mecha-nism/internal flow control technology

分类

航空航天

引用本文复制引用

刘雷,张钊睿,汪昆,王志豪,朱晨,谭慧俊,黄河峡..边界层吸入式进气道气动设计及流动控制技术研究进展[J].航空学报,2026,47(7):1-33,33.

基金项目

国家自然科学基金(12372294) (12372294)

南航"前瞻布局科研专项"重大集成项目(QZJC202401) National Natural Science Foundation of China(12372294) (QZJC202401)

Major Integration Project of the Special Scientific Research Program for Forward-Looking Layout of Nanjing University of Aeronautics and Astronautics(QZJC202401) (QZJC202401)

航空学报

1000-6893

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