Effect of bulk viscosity in supersonic flow past spacecraft

被引：28

作者：

Chikitkin, A. V. ^{[1
]}

Rogov, B. V. ^{[1
,2
]}

Tirsky, G. A. ^{[1
,3
]}

Utyuzhnikov, S. V. ^{[1
,4
]}

机构：

[1] Moscow Inst Phys & Technol, Dolgoprudnyi 141700, Moscow Region, Russia

[2] Russian Acad Sci, MV Keldysh Appl Math Inst, Moscow 125047, Russia

[3] Moscow MV Lomonosov State Univ, Inst Mech, Moscow 119192, Russia

[4] Univ Manchester, Sch Mech Aerosp & Civil Engn, Manchester M13 9PL, Lancs, England

来源：

APPLIED NUMERICAL MATHEMATICS | 2015年 / 93卷

关键词：

Bulk viscosity; Shock wave structure; Parabolized Navier-Stokes equations; Global iterations; Flow past blunt bodies; ABSORPTION;

D O I：

10.1016/j.apnum.2014.01.004

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

In this paper, we consider the effect of bulk viscosity in various hydrodynamic problems. We numerically study this effect on the front structure of the one-dimensional stationary shock wave and on the flow past blunt body. We estimate the effect of the bulk viscosity coefficient (BVC) on the heat transfer and drag of a sphere in a supersonic flow, apparently for the first time, by the numerical solution of parabolized Navier-Stokes equations. The solution is obtained by an original fast convergent method of global iterations of the longitudinal pressure gradient. The directions of further investigations of bulk viscosity are suggested. (C) 2014 IMACS. Published by Elsevier B.V. All rights reserved.

引用

页码：47 / 60

页数：14

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