It has been suggested that the switching of an attaching jet in a wall-attachment fluidic device is directly dependent on the jet deflection. Nevertheless, it seems that the deflection is not sufficiently investigated. In the existing analyses, the parameters, which are obtained experimentally and affected by the geometry of the device, are used. It is desirable that this class of parameter has a well defined physical meaning and is not affected by the geometry.
In this report, the free jet deflection, which is the most basic problem of the jet deflection, is examined experimentally and theoretically. The following matters are confirmed. The main jet momentum at the exit decreases in comparison with the jet without control flow, owing to the pressure rise in the interaction region. On the other hand, the momentum increases due to control flow at downstream. And the so-called discharge coefficient at the flow passage, formed by the main jet and the control nozzle edge, is equal to unity for a small control nozzle setback, while the coefficient is not equal to unity for a large setback, but is much affected by the geometry.
According to the above results, two mathematical models are suggested for the small and large control nozzle setbacks, respectively. For the small setback, the discharge coefficient which is equal to unity, is used. For the large setback, the recovery factor is introduced, which describes the degree of converting the pressure in the interaction region into the momentum at downstream, because the discharge coefficient is very dependent on the geometry.
The results predicted by these models are satisfactory. And the used recovery factor is little affected by the setback.
However, the applicability of the suggested models may be geometrically limited, due to the assumption of uniform, pressure distribution in the interaction region.
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