Scaling law for supersonic core length in circular and elliptic free jets

被引:12
|
作者
Perumal, Arun Kumar [1 ]
Rathakrishnan, Ethirajan [1 ]
机构
[1] Indian Inst Technol Kanpur, Dept Aerosp Engn, Kanpur 208016, Uttar Pradesh, India
关键词
INFRARED SIGNATURE; TRIANGULAR TABS; NOISE FIELD; FLOW;
D O I
10.1063/5.0051872
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We present here the experiments demonstrating the scaling law for supersonic core length in circular and elliptic free jets. A proper scale for the supersonic core length of free jets is found as L c *</mml:msubsup> <mml:msqrt> A R</mml:msqrt> e - 0.11 gamma M j 2</mml:msubsup>, where L c * is the core length normalized by nozzle throat diameter D-th, AR is the aspect ratio of the elliptic nozzle, gamma is the specific heats ratio, and M-j is the ideally expanded jet Mach number. The scaling law developed for supersonic core length shows a close dependence with nozzle expansion ratio <mml:msub> p e / <mml:msub> p a and agrees well with the results reported in open literature, including the data reported for gamma =1.28-1.67. In spite of their uniqueness, the present results refer to circular and elliptic jets only. Thus, other similar studies on rectangular and square jets for a wide range of parameters are needed for a full comprehension of the universality of the scaling law for non-circular jets.
引用
收藏
页数:7
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