An axisymmetric 'fluidic' nozzle to generate jet precession

被引:85
|
作者
Nathan, GJ [1 ]
Hill, SJ [1 ]
Luxton, RE [1 ]
机构
[1] Univ Adelaide, Dept Mech Engn, Adelaide, SA 5005, Australia
关键词
D O I
10.1017/S002211209800202X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A continuously unstable precessing flow within a short cylindrical chamber following a large sudden expansion is described. The investigation relates to a nozzle designed to produce a jet which achieves large-scale mixing in the downstream field. The inlet flow in the plane of the sudden expansion is well defined and free from asymmetry. Qualitative flow visualization in water and semi-quantitative surface flow visualization in air are reported which identify this precession within the chamber. Quantitative simultaneous measurements from fast-response pressure transducers at four tapping points on the internal walls of the nozzle chamber confirm the presence of the precessing field. The investigation focuses on the flow within the nozzle chamber rather than that in the emerging jet, although the emerging flow is also visualized. Two flow modes are identified: a 'precessing jet' mode which is instantaneously highly asymmetric, and a quasi-symmetric 'axial jet' mode. The precessing jet mode, on which the investigation concentrates, predominates in the geometric configuration investigated here. A topologically consistent flow held, derived from the visualization and from the fluctuating pressure data, which describes a three-dimensional and time-dependent precessing motion of the jet within the chamber is proposed. The surface flow visualization quantifies the axial distances to lines of positive and negative bifurcation allowing comparison with related flows involving large-scale precession or flapping reported by others. The Strouhal numbers (dimensionless frequencies) of these flows are shown to be two orders of magnitude lower than that measured in the shear layer of the jet entering the chamber. The phenomenon is demonstrated to be unrelated to acoustic coupling.
引用
收藏
页码:347 / 380
页数:34
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