CALCULATION OF TRANSONIC FLOW PAST THE AFTER-PART OF A PLANE OR AXISYMMETRICAL BODY

被引：0

作者：

SHCHERBAKOV, SA

机构：

来源：

USSR COMPUTATIONAL MATHEMATICS AND MATHEMATICAL PHYSICS | 1989年 / 29卷 / 05期

关键词：

D O I：

10.1016/0041-5553(89)90181-X

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

On the basis of a modified Godunov finite-difference scheme, a method is given for calculating the transonic flow of an ideal gas past the after-part of a plane or axisymmetric elongated body with large angles of inclination and breaks in the generators. Differences schemes adapted to the flow singularities are used, and a new version of the scheme is realized. Relations for the transonic flow remote from the body are obtained in the linear approximation.

引用

页码：75 / 83

页数：9

共 41 条

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