Review and prospect of research on scramjet

被引：0
|
作者：
Liu X. [1 ]
Wang M. [1 ]
Liu J. [1 ]
Ren X. [1 ]
Zhang X. [1 ]
机构：
[1] Beijing Power Machinery Institute, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷 / 05期
关键词：
hypersonic; regenerative cooling; scramjet; supersonic combustion; ultra-high temperature structure;
D O I：
10.7527/S1000-6893.2023.29878
中图分类号：
学科分类号：
摘要：
Since the 1950s，scramjet has been regarded as a goal of the hypersonic propulsion system in the aero⁃ space field，and extensive research work has been conducted in both theory and practical technology. At the begin⁃ ning of the 21st century，the United States made a series of technological breakthroughs close to practical applica⁃ tions，pushing the research and application of the scramjet technology to a new stage. This paper briefly describes the working principle of the scramjet，discusses the difficulties and latest progress in key technologies such as dual-mode working process，hypersonic compression flow，supersonic combustion，ultra-high temperature structure and thermal protection，ground test and numerical simulation，and expounds the understanding and suggestions on the develop⁃ ment direction of key technologies such as wide speed range，repeatability，and higher Mach number of scramjet. © 2024 Chinese Society of Astronautics. All rights reserved.
引用
收藏
相关论文
共 161 条
  • [1] PRISELL E., The scramjet：A solution for hypersonic aerodynamic propulsion, Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, (2005)
  • [2] SEEBASS A R., Review and evaluation of the air force hypersonic technology program：AFSB TR-J-97-01-A ［R］, (1998)
  • [3] Thermal-structural design study of an airframe-integrated scramjet final report, (1980)
  • [4] LIU X Y., Scramjet technology［J］, Winged Missiles Jour⁃ nal, 2, pp. 38-42, (2003)
  • [5] CHEN F D., Review of the development of hypersonic weapons abroad in 2022［J］, Aerospace China, 2, pp. 31-37, (2023)
  • [6] CONNORS J F, MEYERS R C., Design criteria for axi⁃ symmetric and two-dimensional supersonic inlets and ex⁃ its：NACA TN-3589［R］, (1956)
  • [7] MOLDER S, PAISLEY T W., A comparison of three hypersonic air inlets［R］, (1991)
  • [8] RAUSCH D R., Hyper-X program status：AIAA-2001-1910［R］, (2001)
  • [9] NGUYEN L T，, Et al., NASA hypersonic flight demonstrators—Overview，sta⁃ tus，and future plans［J］, Acta Astronautica, 55, 3-9, pp. 619-630, (2004)
  • [10] TREXLER C A., Performance of an inlet for an inte⁃ grated scramjet concept［J］, Journal of Aircraft, 11, 9, pp. 589-591, (1974)
12345678910