期刊
AEROSPACE SCIENCE AND TECHNOLOGY
卷 43, 期 -, 页码 343-349出版社
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2015.03.018
关键词
Flow control; Supersonic flow; Microwave discharge; Laser discharge; Richtmyer-Meshkov instability; Vortex structure
资金
- Scientific Research Program of Dorodnicyn Computing Centre of RAS
- Russian Foundation for Basic Research [15-01-04635a]
The models of energy deposition in an oncoming flow via heated rarefied channel/channels (filaments) are used for consideration of the effect of microwave and laser discharge energy deposition on supersonic flows past combined cylinder bodies. Flow details accompanying streamlining bodies hemisphere-cylinder and hemisphere-cone-cylinder are simulated numerically for an inviscid perfect gas at Mach 2.1 and 3.45. Unsteady vortex structures caused by the Richtmyer-Meshkov instability together with a rarefaction wave reflection are shown to be the reasons for the reduction in stagnation pressure. Optimization of the shape and parameters of heat spot areas resulting from MW and laser energy deposition have been realized on the basis of flow analysis and comparison with experimental data. Estimations of the value of energy needed for generating the heated gas area with the obtained parameters are provided. (C) 2015 Elsevier Masson SAS. All rights reserved.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据