Computational fluid dynamics;
Real gas;
Nozzle;
Plasmatron;
Energy supply;
Shock wave;
NUMERICAL-SIMULATION;
IMPLEMENTATION;
DEPOSITION;
ALGORITHMS;
EQUATIONS;
CHANNEL;
AIR;
D O I:
10.1016/j.camwa.2019.12.015
中图分类号:
O29 [应用数学];
学科分类号:
070104 ;
摘要:
When gas flows at a high speed in a channel with a variable cross sectional area and high-intensity energy supply, it experiences complicated physical and chemical processes producing high-temperature gas effects. High-temperature gas effects are a key issue related to design and optimization of nozzles of plasmatron of alternating current. The finite volume method is applied to solve unsteady compressible Euler equations with high-temperature gas effects. Solutions of some benchmark test cases are reported, and comparison between computational results of chemically equilibrium and perfect air flow-fields is performed. The results of numerical simulation of one-dimensional and two-dimensional under- and over-expanded nozzle flows with a moving region of energy supply are presented. Output nozzle parameters are calculated as functions of a number and time of burning of plasmatron arcs. The results obtained show a qualitative pattern of gas dynamics and thermal processes in the nozzle with unsteady energy supply demonstrating the displacement of the nozzle shock wave towards the nozzle outlet in the over-expanded nozzle flow in comparison to perfect gas flow. (C) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页码:702 / 724
页数:23
相关论文
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[1]
Anderson J. D., 2019, Hypersonic and High-Temperature Gas Dynamics, V3