期刊文献+

Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation 被引量:2

Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation
原文传递
导出
摘要 For achieving high-speed requirement of underwater vehicle,a conceptual engine,which utilizes the hydroreactive characteristic of several metals under supercavitation environment,has been put forward. Especially,in order to obtain specific impulse as great as possible,a dual water injection system is taken into account. Then thermodynamic cycle model,which lead the improvement of power plant and energy system,is introduced in detail,and thermal efficiency is also analyzed. Furthermore,for investigating the performance of this kind of engine system,detailed thermodynamic calculation and analysis are achieved. Especially,regarding hydroreactive metal fuel Mg/AP/HTPB as our target fuel-rich propellant,considering its obvious deficient oxygen property and the energy property of magnesium/water reaction,theoretical calculation method is established by integrating chemical non-equilibrium with chemical equilibrium. Accordingly,low limit of primary water/fuel ratio is determined. In addition,the qualitative and quantitative relationship of performance parameters,such as theoretical specific impulse,nozzle exit temperature,characteristic velocity,etc.,versus water/fuel ratio is investigated respectively. For achieving high-speed requirement of underwater vehicle,a conceptual engine,which utilizes the hydroreactive characteristic of several metals under supercavitation environment,has been put forward. Especially,in order to obtain specific impulse as great as possible,a dual water injection system is taken into account. Then thermodynamic cycle model,which lead the improvement of power plant and energy system,is introduced in detail,and thermal efficiency is also analyzed. Furthermore,for investigating the performance of this kind of engine system,detailed thermodynamic calculation and analysis are achieved. Especially,regarding hydroreactive metal fuel Mg/AP/HTPB as our target fuel-rich propellant,considering its obvious deficient oxygen property and the energy property of magnesium/water reaction,theoretical calculation method is established by integrating chemical non-equilibrium with chemical equilibrium. Accordingly,low limit of primary water/fuel ratio is determined. In addition,the qualitative and quantitative relationship of performance parameters,such as theoretical specific impulse,nozzle exit temperature,characteristic velocity,etc.,versus water/fuel ratio is investigated respectively.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2010年第5期1129-1138,共10页 Journal of Aerospace Power
基金 Supported by National Natural Science Foundation of China (No .50776070) New Teacher Research Support Program of Xi an Jiaotong University (No .0106-08142002)
关键词 hydroreactive metal fuel water ramjet thermodynamic cycle thermal efficiency specific impulse hydroreactive metal fuel water ramjet thermodynamic cycle thermal efficiency specific impulse
  • 相关文献

参考文献7

二级参考文献32

  • 1董师颜 孙思诚 等.固体火箭发动机原理[M].北京:国防工业出版社,1983..
  • 2[1]Lee W M. Aluminum Powder/Water Reaction Ignited by Electrical Pulsed Power, 1993,(8).
  • 3[2]Foote J P,Lineberry J T,Thompson B R,AIAA 96-3086.
  • 4郑邯勇.铝水推进系统的现状与发展前景[J].水中兵器,2002,:175-178.
  • 5[1]Cohen N S.Combustion considerations in fuel-rich propellant systems.AIAAJ V,July 1969,7(7):1345-1352
  • 6[2]Chen D M,Luh S P.Combustion study of boron-based fuel-rich solid propellant.Combustion of boron-based solid fuels and propellants in propulsion systems,edited by Kuo K K,1993
  • 7[3]李宜敏,张中钦等.固体火箭发动机原理.北京:北京航空航天大学出版社,1991
  • 8[4]Meinkohn Dirk.Boron Particle ignition in a restricted thermodynamical equilibrium. AIAAJ V,21(7):1006-1007
  • 9Kuehl D K. Ignition and combustion of aluminum and beryllium[J]. AIAA J. 1965, 3(12).
  • 10Kiely D H. Review of underwater thermal propulsion [ C ].Joint Propulsion Conference July 1-3,1966, Lake Buena Vista,FL.

共引文献87

同被引文献12

引证文献2

二级引证文献5

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