首页> 外文期刊>Acta astronautica >Integration of modeling and simulation of warm pressurization and feed systems of liquid propulsion systems
【24h】

Integration of modeling and simulation of warm pressurization and feed systems of liquid propulsion systems

机译:液体推进系统的热增压和进料系统建模与仿真的集成

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper, a new approach for simultaneous simulation of warm pressurization systems and an engine feed system is developed. The governing equations of the pressurization system are also derived. The simulation results of gas generator pressure, ullage pressure, and pressure at the inlet of the fuel and oxidizer pumps are compared with experimental results. This comparison reveals that the developed approach may successfully be used to determine the interaction effects of an engine feed system and an engine pressurization system. At present, the approach and results are limited to single stage to orbit liquid engines that use the gas generator gases for pressurization.
机译:在本文中,开发了一种同时模拟热增压系统和发动机进气系统的新方法。还推导了增压系统的控制方程。将气体发生器压力,空载压力以及燃料和氧化剂泵入口处的压力的模拟结果与实验结果进行了比较。该比较表明,所开发的方法可以成功地用于确定发动机进给系统和发动机增压系统的相互作用效果。目前,方法和结果仅限于使用气体发生器气体进行增压的单级至轨道液体发动机。

著录项

  • 来源
    《Acta astronautica》 |2011年第6期|p.258-265|共8页
  • 作者单位

    Faculty of Aerospace Engineering, K.N.T. University of Technology, Tehran 1656983911, Iran;

    Materials, Mechanics and Structures Research Division, Faculty of Engineering, The University of Nottingham—Malaysia Campus,43500 Semenyih, Selangor, Malaysia;

    Faculty of Aerospace Engineering, K.N.T. University of Technology, Tehran 1656983911, Iran;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    mathematical modeling; pressurization; gas generator; turbo-pump; liquid propellant tanks; gas mixer;

    机译:数学模型增压气体发生器涡轮泵液体推进剂罐气体混合器;

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