Statistical simulation of high-altitude aerodynamic problems

被引：0

作者：

Ivanov, MS ^{[1
]}

Markelov, GN ^{[1
]}

Kashkovsky, AV ^{[1
]}

Gimelshein, SF ^{[1
]}

机构：

[1] Russian Acad Sci, Inst Theoret & Appl Mech, Novosibirsk 630090, Russia

来源：

PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES | 1999年 / 420卷

关键词：

DSMC; local bridging; SMILE system;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The paper presents a multi-purpose computational system SMILE based on statistical methods of computational rarefied gas dynamics and aimed at the study of different aerodynamic problems in regimes from free molecular through transitional to continuum. The results of application of SMILE to investigation of flows about X38 model geometry, reentry capsule Soyuz, and space station Mir are presented. An engineering approach based on local bridging is also used to calculate aerodynamic characteristics of Soyuz and Mir in free molecular and transitional regimes.

引用

页码：245 / 252

页数：8

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