Analytical Shock Jump Formulae for Cryogenic Homogeneous Two-Phase Nozzle Flow

By I.Sinan Akmandor; Toshio Nagashima

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Analytical Shock Jump Formulae for Cryogenic Homogeneous Two-Phase Nozzle Flow

机译：低温均相两相喷嘴流的激波解析公式

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Choked flux rates and shock jump relations were calculated both analytically and computationally for a converging-diverging nozzle. High inlet stagnation pressure with a maximum of 6.45Mpa was applied to the cryogenic vapor-liquid nitrogen flow. The total inlet-to-static exit pressures ratio range between 3.5 and 15.3. The analytical shock jump expressions, which were derived, are exact extensions of the Rankine-Hugoniot Single-phase gas dynamic relations.

机译：对于收敛-发散喷嘴，通过分析和计算来计算节流通量率和激波跳跃关系。将最高为6.45Mpa的高入口停滞压力施加到低温气液氮流中。总的入口与静态出口压力之比在3.5和15.3之间。推导的解析激波跳跃表达式是Rankine-Hugoniot单相气体动力学关系的精确扩展。

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来源
《Transactions of the Japan society for aeronautical and space sciences》 |2000年第140期|p.67-76|共10页
作者
By I.Sinan Akmandor; Toshio Nagashima;
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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
中图分类航空;
关键词
Two-Phase Flow; Homogeneous; Cryogenic Nitrogen;

机译：两相流;同质;低温氮;

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专利

1. Newton-Raphson solution of cryogenic homogeneous two-phase flow in convergent-divergent nozzles [J] . I.Sinan Akmandor, Toshio Nagashima Transactions of the Japan Society for Aeronautical and Space Sciences . 1997,第127期

机译：会聚-发散喷嘴中低温均质两相流的牛顿-拉夫森解
2. On the stability of stationary shock waves in nozzle flows with homogeneous condensation [J] . Delale CF., van Dongen MEH., Lamanna G. Physics of fluids . 2001,第9期

机译：关于稳定冲击波在喷嘴流中具有均匀凝结的稳定性
3. Explicit critical pressure ratio for choked two-phase homogeneous nozzle flow [J] . Moncalvo D, Friedel L Chemical Engineering & Technology: Industrial Chemistry -Plant Equipment -Process Engineering -Biotechnology . 2007,第4期

机译：两相均相喷嘴堵塞的显式临界压力比
4. Numerical Simulation of Homogeneous Equilibrium Two-Phase Flows with Shock-Stable Schemes [C] . Seung-Won Ihm, Seok Woo Hong, Sangho Han, AIAA Computational Fluid Dynamics Conference . 2007

机译：具有冲击稳定方案的均匀平衡两相流量的数值模拟
5. An experimental investigation of supersonic rectangular over-expanded nozzle of single and two-phase flows. [D] . Ibrahim, Ashraf Elsaid Mohamed. 2008

机译：单相和两相流超声速矩形过膨胀喷嘴的实验研究。
6. Pressure drop of two-phase helium along long cryogenic flexible transfer lines to support a superconducting RF operation at its cryogenic test stand [O] . M. H. Chang, M. H. Tsai, Ch. Wang, -1

机译：沿长低温柔性传输线的两相氦的压降以在其低温测试台上支持超导RF操作
7. On the stability of stationary shock waves in nozzle flows with homogeneous condensation [O] . Delale, CF, Lamanna, G Grazia, Dongen, van, MEH Rini 2001

机译：关于稳定冲击波在喷嘴流中具有均匀凝结的稳定性
8. TWO-PHASE CHOKED FLOW OF CRYOGENIC FLUIDS IN CONVERGING-DIVERGING NOZZLES [R] . Robert J. Simoneau, Robert C. Hendricks 1979

机译：收敛 - 分散喷嘴中低温流体的两相CH流

Analytical Shock Jump Formulae for Cryogenic Homogeneous Two-Phase Nozzle Flow

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