INVISCID STEADY UNSTEADY-FLOW CALCULATIONS

被引：0
|
作者：
PORDAL, HS
KHOSLA, PK
RUBIN, SG
机构：
[1] Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati
来源：
COMPUTERS & FLUIDS | 1991年 / 19卷 / 01期
基金：
美国国家航空航天局;
关键词：
D O I：
10.1016/0045-7930(91)90009-7
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
The solution of the Euler equations using a flux splitting procedure is considered for low subsonic to high supersonic flows. Steady and unsteady, internal and external flow fields, are computed. For transient flows, a direct sparse matrix solver is applied to compute the flow field at each instant of time. Oscillation free normal and oblique shocks are captured. Unstart and restart of a simplified two-dimensional inlet is investigated.
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页码：93 / 118
页数：26
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