首页> 外文会议>International symposium on liquid rocket propulsion >Liquid-propellant droplet vaporization and combustion
【24h】

Liquid-propellant droplet vaporization and combustion

机译:液体推进剂液滴蒸发和燃烧

获取原文

摘要

The physico-chemical processes in a liquid-rocket combustion chamber are extremely complicated, involving an array of intricacies such as jet atomization, spray formation, droplet transport, multiphase flow mixing, and chemical reactions. Many strong interactions among these processes with wide disparity in time and length scales exist in close proximity to one another. Since the transport characteristics of individual droplest play a decisive role in determining the local flow behavior in a spray field, the study of droplet vaporization and combustion were given by Williams, Faeth, Law, Sirignano, and Dwyer.
机译:液体火箭燃烧室中的物理化学方法非常复杂,涉及诸如喷射雾化,喷雾形成,液滴传输,多相流动和化学反应的复杂阵列。 这些过程之间的许多强的相互作用在时间和长度较大的情况下,彼此紧密地存在。 由于个体变动的运输特性在确定喷雾场中的局部流动行为时起着决定性作用,因此威廉姆斯,粮农组织,法律,苏里尼亚诺和Dwyer对液滴汽化和燃烧的研究。

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