首页> 外文期刊>Russian Aeronautics >Numerical Simulation of the Flow in the Scramjet Combustion Chamber Taking into Account Nonequilibrium Chemical Reactions
【24h】

Numerical Simulation of the Flow in the Scramjet Combustion Chamber Taking into Account Nonequilibrium Chemical Reactions

机译:考虑到非核状化学反应的汽轮燃烧室流量的数值模拟

获取原文
获取原文并翻译 | 示例
       

摘要

A method for numerical simulation of the combustion of hydrogen in a supersonic air flow is developed. Comparison of the calculation results with the experimental data showed a satisfactory agreement. The calculation results using the nonequilibrium and equilibrium techniques differ from each other. It is shown that combustion parameters substantially depend on the geometric characteristics of the inlet device, the combustion chamber and the nozzle.
机译:开发了一种用于超声波空气流中氢燃烧的数值模拟的方法。 计算结果与实验数据的比较显示了令人满意的协议。 使用非质量和平衡技术的计算结果彼此不同。 结果表明,基本上取决于入口装置的几何特性,燃烧室和喷嘴的燃烧参数。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号