Experimental production of two-dimensional shock waves of arbitrary profile

被引:10
|
作者
Skews, B. [1 ]
Gray, B. [1 ]
Paton, R. [1 ]
机构
[1] Univ Witwatersrand, Sch Mech Ind & Aeronaut Engn, ZA-2050 Johannesburg, South Africa
基金
新加坡国家研究基金会;
关键词
Gas dynamics; Shock wave; Shock tube;
D O I
10.1007/s00193-014-0541-4
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A concept has been developed, and implemented, where the initial shape of a shock wave can, within limits, be arbitrarily set, with a fixed pressure ratio across it, and the duct into which it propagates can also be arbitrarily defined. A narrow slit is positioned on the end wall of a shock tube and is supplied by the essentially constant pressure behind the reflected wave from the shock tube operation. The wave propagating through the slit then enters a narrow test section positioned perpendicular to the main shock tube axis. Initial studies were for a converging cylindrical shock segment, followed by examples of more complex profiles producing waves having both converging (increasing strength), and diverging (decreasing strength) components.
引用
收藏
页码:1 / 10
页数:10
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