Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections

被引：29
|
作者：
Ivanov, MS [1 ]
Ben-Dor, G
Elperin, T
Kudryavtsev, AN
Khotyanovsky, DV
机构：
[1] Russian Acad Sci, Inst Theoret & Appl Mech, Computat Aerodynam Lab, Siberian Div, Novosibirsk 630090, Russia
[2] Ben Gurion Univ Negev, Dept Mech Engn, Pearlstone Ctr Aeronaut Engn Studies, IL-84105 Beer Sheva, Israel
来源：
AIAA JOURNAL | 2001年 / 39卷 / 05期
关键词：
D O I：
10.2514/2.1406
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Flow-mach-number-variation-induced hysteresis was studied in steady shock wave reflections. The flow between two symmetrically spaced wedges was simulated using a shock-capturing total variation diminishing (TVD) scheme. It was shown that a flow Mach number variation-induced hysteresis is possible in two-dimensional steady flows.
引用
收藏
页码：972 / 974
页数：3
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