通道内多组分反应气体不连续非定常流动的网格特征计算方法

IF 1.8 Q3 MECHANICS
Fluids Pub Date : 2023-09-27 DOI:10.3390/fluids8100265
Vladimir Gidaspov, Natalia Severina
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引用次数: 0

摘要

本文描述了模拟多组分反应气体的准一维非定常流动的计算算法。该建模技术的特殊性在于强弱不连续面路径为移动计算节点,其参数采用特殊算法计算。开发了一套程序,可用于解决有应用价值的反应气体动力学问题,也可作为物理气体动力学培训课程的插图。本文给出了在力学问题研究所和物理与技术研究所的实验设备上对平面通道内超声速流动进行数值模拟的结果。计算结果与实验结果吻合较好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Grid-Characteristic Method for Calculation of Discontinuous Non-Steady Flows of a Multicomponent Reacting Gas in Channels
This paper is devoted to the description of computational algorithms for modeling quasi-one-dimensional non-steady flows of a multicomponent reacting gas. The particularity of the developed modeling technique is that the paths of strong and weak discontinuities are mobile computational nodes, and the parameters for them are calculated using special algorithms. A set of programs has been developed, which can be used to solve the problems of the reacting gas dynamics that are of applied importance, as well as serve as an illustrator for physical gas dynamics training courses. The paper provides the results of the numerical modeling of the supersonic flow in a flat channel simulating the operation of experimental facilities of the Institute for Problems in Mechanics and the Institute of Physics and Technology. A satisfactory correlation between the calculated and experimental data has been obtained.
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来源期刊
Fluids
Fluids Engineering-Mechanical Engineering
CiteScore
3.40
自引率
10.50%
发文量
326
审稿时长
12 weeks
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