Research status and development trend of air-breathing high-speed vehicle/ engine integration

被引:2
|
作者
Luo, Shibin [1 ,2 ]
Sun, Yuhang [1 ]
Liu, Jun [2 ]
Xie, Xun [2 ]
Tian, Jiaqi [1 ]
Song, Jiawen [2 ]
机构
[1] Cent South Univ, Sch Automat, Changsha 410083, Peoples R China
[2] Cent South Univ, Res Inst Aerosp Technol, Changsha 410083, Peoples R China
关键词
Wide-range aircraft/engine integration; Airframe/engine integration; Aerodynamics/propulsion integration; Air-breathing hypersonic vehicle; Hypersonic vehicle design; SCRAMJET NOZZLE; DESIGN METHOD; COMBUSTION CHARACTERISTICS; AERODYNAMIC CONFIGURATION; OPTIMIZATION DESIGN; HYPERSONIC INLET; WAVERIDER; EXPANSION; JET; METHODOLOGY;
D O I
10.1016/j.ast.2024.109675
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Air-breathing vehicles, a crucial field of the aerospace industry in recent years, are required to have exceptional flight performance in a wide range. As a practical and essential way to realize efficient flight, the integration design emerges as a prominent characteristic of air-breathing vehicles. This article reviews and analyzes the design connotation, critical progress, and technical attributes of high-speed air-breathing integration vehicles, including supersonic aerodynamics/propulsion integration, hypersonic cruise-type airframe/engine integration, and wide-range aircraft/engine integration. In the supersonic aerodynamics/propulsion integrated design phase, creating a vehicle with excellent maneuverability and stealth performance has become the design focus. While in the hypersonic cruise-type airframe/engine integrated design phase, designers proposed various rotational symmetrical slender body and lifting-body configurations to match the scramjet engines. This provided strong support for breaking through thrust-drag matching in hypersonic cruise. For wide-range aircraft/engine integration vehicles, a more complex service environment imposes higher requirements on their levels of integration. The progression from supersonic aerodynamics/propulsion integration to hypersonic cruise-type airframe/engine integration, and further to wide-range aircraft/engine integration, signifies the exploration of air-breathing aircraft towards wider speed range and broader airspace. Finally, a detailed analysis of the distinctions among these three types of integrated vehicles is presented, and the development proposals and trends of wide-range aircraft/engine integration vehicles are discussed.
引用
收藏
页数:40
相关论文
共 50 条
  • [1] Status and development trend of the guidance and control for air-breathing hypersonic vehicle
    Fang, Yangwang
    Chai, Dong
    Mao, Donghui
    Zhang, Lei
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2014, 35 (07): : 1776 - 1786
  • [2] High-speed air-breathing propulsion
    Ladeinde, Foluso
    Dalton, Jeff
    AEROSPACE AMERICA, 2012, 50 (11) : 50 - 50
  • [3] High-speed air-breathing propulsion
    Kaemming, Tom
    AEROSPACE AMERICA, 2009, 47 (11) : 37 - 37
  • [4] Status and problems of development of technology for detonation pulsating air-breathing jet engine
    Remeev, N.Kh.
    Vlasenko, V.V.
    Khakimov, R.A.
    Ivanov, V.V.
    Khimicheskaya Fizika, 2001, 20 (07): : 119 - 130
  • [5] HIGH-SPEED TRACKED AIR CUSHION VEHICLE (TACV) RESEARCH AND DEVELOPMENT
    LAMPROS, AF
    MECHANICAL ENGINEERING, 1973, 95 (10) : 76 - 77
  • [6] Engine idle speed control research status and development trend
    Yin Fengfeng
    Sun Jianmin
    Wang Wenwen
    PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON MECHATRONICS, MATERIALS, CHEMISTRY AND COMPUTER ENGINEERING 2015 (ICMMCCE 2015), 2015, 39 : 1884 - 1888
  • [7] Research Status and Development Trend of Asphalt Concrete Structure of High-speed Railway Subgrade
    Cai D.
    Ye Y.
    Lou L.
    Shi Y.
    Pang S.
    Tiedao Xuebao/Journal of the China Railway Society, 2022, 44 (10): : 112 - 122
  • [8] Nonlinear control of an air-breathing engine including its validation with vehicle guidance
    Maity, Arnab
    Rajasekaran, Jagannath
    Padhi, Radhakant
    AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 45 : 242 - 253
  • [9] Distinctive Features of the Flow past a Flight Vehicle Integrated with an Air-Breathing Engine at High Supersonic Velocities
    N. A. Blagoveshchenskii
    V. N. Gusev
    S. M. Zadonskii
    Fluid Dynamics, 2004, 39 : 649 - 656
  • [10] Distinctive Features of the Flow past a Flight Vehicle Integrated with an Air-Breathing Engine at High Supersonic Velocities
    Blagoveshchenskii, N. A.
    Gusev, V. N.
    Zadonskii, S. M.
    FLUID DYNAMICS, 2004, 39 (04) : 649 - 656