Experimental and computational visualization and frequency measurements of the jet oscillation inside a fluidic oscillator

Journal of Visualization - Tập 5 - Trang 263-272 - 2002
O. Uzol1, C. Camci1
1Department of Aerospace Engineering, Pennsylvania State University, University Park, USA

Tóm tắt

PIV measurements and computational simulations (2D, unsteady Navier-Stokes) are performed to visualize the inherently unsteady jet oscillation inside a fluidic oscillator. Both the measurements and computations are obtained for a jet exit Reynolds number of 321, based on the maximum velocity and the nozzle width at the jet exit plane. The computed jet oscillation frequency is in close agreement with the measured PIV frequency. Formation of a pressure gradient across the jet is observed from the computations. The variation of the jet oscillation frequency with jet exit Reynolds number is also determined by single sensor hot-wire measurements inside the oscillation chamber.

Tài liệu tham khảo

Bauer, P., Fluidic Oscillator and Spray Forming Output Chamber, United States Patent No. 4,184,636 (1980).

Bauer, P., Fluidic Oscillator Flowmeter, United States Patent No. 4,244,230 (1981).

FIDAP 7.0, Users Manual, Fluid Dynamics International Inc. (1993).

Huang, B. T., Flowmeter Having a Fluidic Oscillator, United States Patent No. 5,396,809 (1995).

Huang, B. T. and Hocquet, J., Fluidic Oscillator, United States Patent No. 5,396,808 (1995).

Mansy, H. and Williams, D. R., An Experimental and Numerical Study of Trapped Vortex Pair Fluidic Flowmeter, ASME FED Forum on Turbulent Flows, 76 (1989), 35–39.

Parry, A. J., Chiwanga, S. G., Kalsi, H. S. and Jepson, P., Numerical and Experimental Visualization of Flow through a Target Fluidic Oscillator, ASME FED Experimental and Numerical Flow Visualization, 128 (1991), 327–334.

Uzol, O., Novel Concepts and Geometries as Alternatives to Conventional Circular Pin Fins for Gas Turbine Blade Cooling Applications, Ph.D. Thesis, Pennsylvania State University, University Park, PA, USA (2000).