Brief communicationThe influence of inlet flow condition on the frequency of self-excited jet precession
Introduction
A continuous precession of an initially axisymmetric jet has been observed within a short cylindrical chamber following a large sudden expansion (Hallett and Gunther, 1984; Dellenback et al., 1988; Nathan et al., 1998). Distinct from a swirling motion, the precession of a jet refers to a “gyroscopic-like” motion of the entire jet about an axis in space other than its own centerline. The patented, wholly axisymmetric nozzle to generate such a precessing jet (PJ) flow, see Fig. 1, is characterized by a small inlet (diameter=d), a large chamber (diameter=D; length=L) and an outlet lip (Luxton and Nathan, 1988; Nathan et al., 1998). The configuration of the device must be within specific geometric ratios, namely and L/D=2–3.5 to enable the jet precession. The flow within the chamber is nevertheless bistable, so that an axisymmetric flow mode can also be generated, and the probability, or prevalence, of the precessing mode depends upon these ratios (Nathan et al., 1998). However, when an axisymmetric center-body (C-B) is mounted upstream of the outlet lip (Wong et al., 2003), the probability of precession is effectively unity, provided that the Reynolds number (where Ub is the bulk mean velocity of the jet at the inlet exit) is sufficiently high.
The PJ flow within the nozzle chamber is complex. Any alteration to the chamber configuration is expected to cause a significant change to the flow behavior such as the precession frequency (fp). Mi et al. (1999) and Mi and Nathan (2000) have investigated the effect of various geometric parameters on fp. They observed that fp increases significantly with increasing L (or Lc). It was also revealed that the precession frequency is even more sensitive to the distance between the C-B and the outlet exit. By comparison, the outlet diameter has little influence on fp.
Wong et al. (2004) have demonstrated that the characteristics of the inlet flow to the chamber influences the probability of precession. Specifically the probability of precession depends on the type of inlet, and is greater with a sharp-edged orifice plate than with a long pipe, and least with a smooth contraction inlet. This indicates the importance of the inflow condition for the occurrence of jet precession. However, the effect of the inlet flow on the precession frequency fp has yet to be investigated, prompting the present study.
In this Brief communication, the effect of different inlet configurations on the precession frequency and Strouhal number is examined. We use three different types of inlet: i.e., smooth contraction, which generates a ‘top-hat’ velocity profile, sharp-edged orifice, which leads to a near-field vena contracta, and a long straight pipe, through which fully developed turbulent pipe flow emerges. Previous investigations of an axisymmetric free jet [e.g., Mi et al., 2001a, Mi et al., 2001b] have shown significant differences between the near-field structures from similar configured nozzles. For instance, there are well-defined large-scale coherent structures in the near field from a smooth contraction, while such structures are considerably smaller and less coherent in the pipe jet. Likewise, the coherent structures in the orifice jet are formed at a considerably higher rate than in the contraction jet. Similar trends are anticipated to occur with such jets confined in a circular chamber. If this is true, the frequency of jet precession could be expected to be different for the three cases. Present measurements of fp will check this speculation.
Section snippets
Experimental details
The geometric ratios of the nozzle have been selected to provide a high probability of precession (Wong et al., 2002). The nozzle system is supplied with filtered and compressed air at pressures of up to 500 kPa at room temperature of approximately 20 °C. The jet exit velocity can be varied by changing the supply pressure. The present study uses two geometrically similar, but different-sized, PJ nozzles, with D=26 mm and 80 mm, respectively. These nozzles all have a C-B with and identical
Results and discussion
Fig. 3 shows the jet precession frequency fp against the Reynolds number , instead of Ub, to provide information about Re although only Ub has been varied. All three inlet configurations have been tested for the large nozzle (), while only the smooth contraction and orifice inlets have been used for the small nozzle (). Several observations can be made immediately. First, the precession frequency fp scales approximately linearly with Ub over the measured range of Re,
Concluding remarks
We have investigated the dependence of a self-excited jet precession within an axisymmetric chamber on the inflow condition from three nozzles of the same diameter but different profiles. It is found that the precession Strouhal number Stp depends on the geometric profile of the inlet nozzle. Specifically for the present cases, Stp with a sharp-edged orifice is approximately double that from a long pipe, and 60% higher than that from a smooth contraction.
Using a mechanically precessing jet
Acknowledgements
The collaborative support of the Australian Research Council and Fuel & Combustion Technology Ltd is gratefully acknowledged.
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