留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation

YANGYa-jing

YANGYa-jing. Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation[J]. 航空动力学报, 2010, 25(5): 1129-1138.
引用本文: YANGYa-jing. Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation[J]. 航空动力学报, 2010, 25(5): 1129-1138.
YANG Ya-jing. Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation[J]. Journal of Aerospace Power, 2010, 25(5): 1129-1138.
Citation: YANG Ya-jing. Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation[J]. Journal of Aerospace Power, 2010, 25(5): 1129-1138.

Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation

基金项目: Supported by National Natural Science Foundation of China (No .50776070);New Teacher Research Support Program of Xi an Jiaotong University (No .0106-08142002)

Theoretical investigation on water/metal fuel ramjet motor-thermodynamic cycle and thermodynamic calculation

Funds: Supported by National Natural Science Foundation of China (No .50776070);New Teacher Research Support Program of Xi an Jiaotong University (No .0106-08142002)
  • 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.

     

  • 加载中
计量
  • 文章访问数:  1515
  • HTML浏览量:  117
  • PDF量:  429
  • 被引次数: 0
出版历程
  • 收稿日期:  2009-02-09
  • 修回日期:  2010-04-06
  • 刊出日期:  2010-05-28

目录

    /

    返回文章
    返回