首页> 外文期刊>Combustion Science and Technology >CRYOGENIC FLUID JETS AND MIXING LAYERS IN TRANSCRITICAL AND SUPERCRITICAL ENVIRONMENTS
【24h】

CRYOGENIC FLUID JETS AND MIXING LAYERS IN TRANSCRITICAL AND SUPERCRITICAL ENVIRONMENTS

机译:穿越和超临界环境中的低温流体射流和混合层

获取原文
获取原文并翻译 | 示例
       

摘要

This paper provides an overview of recent advances in the theoretical modeling and numerical simulation of cryogenic fluid injection and mixing in transcritical and supercritical environments. The basis of the analysis is a general theoretical and numerical framework that accommodates full conservation laws and real-fluid thermodynamic and transport phenomena. All of the thermophysical properties are determined directly from fundamental thermodynamics theories, along with the use of corresponding-state principles. Turbulence closure is achieved using a large-eddy-simulation technique, in which large-scale motions are calculated explicitly and the effects of unresolved small-scale turbulence are modeled either analytically or empirically. The analysis has been applied to study: (1) fluid jet dynamics, (2) swirl injection of liquid oxygen through a simplex swirl injector, and (3) shear co-axial injection and mixing of liquid oxygen and methane. Various effects, including density stratification, shear-layer instability, volume dilatation, and property variations, dictating the evolution of cryogenic jets and mixing layers, are identified and analyzed in depth. The jet dynamics are found to be largely determined by the local thermodynamic state through its influence on the thermophysical properties of the fluid. The impact of injector configuration and operating conditions on the swirl injector behavior are also highlighted. These results not only shed light on the subject problems, but also provide a quantitative basis for identifying the design parameters and flow variables that exert the strongest influence on the underlying processes.
机译:本文概述了跨临界和超临界环境中低温流体注入和混合的理论建模和数值模拟的最新进展。分析的基础是一个通用的理论和数值框架,可容纳全部守恒定律以及实际流体的热力学和传输现象。所有的热物理性质都是直接根据基本的热力学理论确定的,并使用了相应的状态原理。使用大涡模拟技术可实现湍流闭合,其中显式计算了大尺度运动,并通过解析或经验对未解决的小尺度湍流的影响进行了建模。该分析已用于研究:(1)流体射流动力学;(2)通过单工涡旋喷射器对液态氧进行涡旋喷射;(3)剪切同轴注入以及液态氧和甲烷的混合。确定并深入分析了各种影响,包括密度分层,剪切层不稳定性,体积膨胀和特性变化,这些影响决定了低温射流和混合层的演变。发现射流动力学很大程度上取决于局部热力学状态,这取决于其对流体热物理性质的影响。还重点介绍了喷油嘴配置和运行条件对旋流喷油嘴性能的影响。这些结果不仅阐明了主题问题,而且为确定对基础工艺产生最大影响的设计参数和流量变量提供了定量依据。

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