期刊文献+

法俄联合研制的连续爆震波发动机 被引量:2

下载PDF
导出
摘要 介绍了连续爆震波发动机的概念,给出了设计中的关键问题,包括发动机尺寸、平均压强与混合物流率间的关系、热流以及连续爆震波发动机的推力矢量控制。总结了试验过程中获得的主要结果。
出处 《飞航导弹》 北大核心 2007年第6期39-43,共5页 AERODYNAMIC MISSILE JOURNAL
  • 相关文献

参考文献9

  • 1Zel' dovich Ya. B. The Question About Energetic Use of Detonation Combustion. Zh. Tech. Fiz., 1940, V. 10, iss. 17 : 1453-1461
  • 2Nicholls J A, Dabora E K, Gealler R A. Studies in Connection with Stabilized Gaseous Detonations Waves. In the 11th Symposium (International) on Combustion and Detonation, London, 1959 : 766-772
  • 3Voitsekhovskii B V, Mitrofanov V V, Topchiyan M E. Structure of a Detonation Front in Gases. Siberian Branch of the USSR Academy Sci. , Novosibirsk, 1963
  • 4Voitsekhovskii B V. Stationary Spin Detonation. in Soy. J. of Applied Mechanics and Technical Physics. 1960, No3:157-164
  • 5Voitsekhovskii B V. Stationary Detonation. in Soy. J. Doklady USSR Academy Sci., 1959, V. 129, No. 6: 1254-1256
  • 6Bykovskii F A, Mitrofanov V V. Detonative Combustion of Gas Mixture in a Cylindrical Chamber. in Fizika goreniya i vzryva (Combustion, Explosion, and Shock Waves). 1980, V. 16, No5:107-117
  • 7Vasiliev A A, Zak DV. Detonation of Gas Jets. in Fizika goreniya i vzryva (Combustion, Explosion, and Shock Waves). 1986, V. 22, No4:82-88
  • 8Mitrofanov V V. Energy Criterion of Detonation Initiation. in Lavrentyev Readings on Mathematics, Mechanics and Physics, September 18-20, 2000, Novosibirsk, Russia: 139
  • 9Knab O, Fr ohlich A, Wennerberg D, Haslinger W. Advanced Cooling Circuit Layout for the VINCI Expander Cycle Thrust Chamber. AIAA 2002-4005

同被引文献29

  • 1Voitsekhovskii B V. Maintained detonations. Doklady Akademii Nauk UzSSR, 1959.
  • 2Voitsekhovskii B V. Spinning maintained detonations. Prikl. Mekh. Tekh. Fiz., 1960.
  • 3Mikhailov V V, Topchiyan M E. Study of continuous detonation in an annular channel. Fizika Goreniya I Vzryva, 1965.
  • 4Nicholls J A, Cullen R E. The feasibility of a rotating detonation wave rocket motor. Rocket Propulsion Lab. RPL-TDR-64-113, Edwards Air Force Base, California, 1964.
  • 5Nicholls J A, Cullen R E, Ragland K W. Feasibility studies of a rotating detonation wave rocket motor. Journal of Spacecraft, 1996 (3) : 893-898.
  • 6Bykovskii F A, Klopotov I D, Mitrofanov V V. Spin detonation of gases in a cylindrical combustor. Doklady Akademii Nauk UzSSR, 1975(5): 1038-1041.
  • 7Bykovskii F A, Mitrofanov V V. Detonation combustion of a gas mixture in a cylindrical chamber. Combustion, Explosion, and Shock Waves, 1980(16) : 570-578.
  • 8Zhdan S A, Mardashev A M, Mitrofanov V V. Calculation of the flow of spin detonation in annular chamber. Combustion, Explosion, and Shock Waves, 1990 (26) : 210-214.
  • 9Bykovskii F A, Vedernikov E F. Continuous detonation of a subsonic flow of a propellant. Combustion, Explosion, and Shock Waves, 2003 (39) : 323-334.
  • 10Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous spin detonations. Journal of Propulsion and Power, 2006(26) : 1204-1216.

引证文献2

二级引证文献54

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部