Shibin Luo , Yuhang Sun , Jun Liu , Xun Xie , Jiaqi Tian , Jiawen Song
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引用次数: 0
Abstract
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.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
• The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites
• The control of their environment
• The study of various systems they are involved in, as supports or as targets.
Authors are invited to submit papers on new advances in the following topics to aerospace applications:
• Fluid dynamics
• Energetics and propulsion
• Materials and structures
• Flight mechanics
• Navigation, guidance and control
• Acoustics
• Optics
• Electromagnetism and radar
• Signal and image processing
• Information processing
• Data fusion
• Decision aid
• Human behaviour
• Robotics and intelligent systems
• Complex system engineering.
Etc.