Free-flight experiment and numerical simulation for cold thruster plume

被引:19
|
作者
Ivanov, MS
Markelov, GN
Gerasimov, YI
Krylov, AN
Mishina, LV
Sokolov, EI
机构
[1] Russian Acad Sci, Inst Theoret & Appl Mech, Computat Aerodynam Lab, Novosibirsk 630090, Russia
[2] RSC Energia, Aerothermodynam Dept, Korolev 141070, Moscow Region, Russia
[3] Inst High Performance Comp & Data Bases, CFD Lab, St Petersburg 194291, Russia
关键词
D O I
10.2514/2.5460
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An experiment, Astra-2, was performed at the space station Mir in 1995-1996 to study its ambient atmosphere parameters. For far-field plume research, the equipment of Astra-2 included a small cold gas thruster using a marked gas, argon. The results of this research offer a good basis for validation of various numerical approaches for plume flows, from simple engineering models to exact numerical approaches using a Navier-Stokes solver in the continuum regime and a direct simulation Monte-Carlo code in the near-continuum, transitional, and free-molecular regimes. A comparison of experimental and numerical results shows the necessity of accounting for argon condensation processes in the nozzle and in the vicinity near the nozzle.
引用
收藏
页码:417 / 423
页数:7
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