Effects of including compressibility in the numerical modeling of flows produced by and in synthetic jet actuators — consisting of an oscillating diaphragm in a cavity with a small circular orifice in the face opposite the diaphragm — has been studied for axisymmetric configurations. Numerical results obtained on the assumption of incompressible and compressible flows with orifice diameters of the 20 and 40 μm and with an orifice length of 50 μm are compared. There are significant differences between compressible and incompressible flows for the 20 μm orifice, in that the jet velocity is greatly reduced when compressible flow is assumed, whereas the differences are much smaller in the 40 μm case. For both orifices the pressure rise upstream of the orifice is smaller when the fluid is compressible. It follows that results obtained on the assumption of incompressible flow cannot be extrapolated for micro-synthetic jet actuators handling compressible fluids.
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ASME 2004 2nd International Conference on Microchannels and Minichannels
June 17–19, 2004
Rochester, New York, USA
Conference Sponsors:
- Nanotechnology Institute
ISBN:
0-7918-4164-2
PROCEEDINGS PAPER
Compressibility Effects in Micro Synthetic Jets
Victoria Timchenko,
Victoria Timchenko
University of New South Wales, Sydney, Australia
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John Reizes,
John Reizes
University of New South Wales, Sydney, Australia
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Eddie Leonardi
Eddie Leonardi
University of New South Wales, Sydney, Australia
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Victoria Timchenko
University of New South Wales, Sydney, Australia
John Reizes
University of New South Wales, Sydney, Australia
Eddie Leonardi
University of New South Wales, Sydney, Australia
Paper No:
ICMM2004-2345, pp. 273-280; 8 pages
Published Online:
December 2, 2008
Citation
Timchenko, V, Reizes, J, & Leonardi, E. "Compressibility Effects in Micro Synthetic Jets." Proceedings of the ASME 2004 2nd International Conference on Microchannels and Minichannels. ASME 2nd International Conference on Microchannels and Minichannels. Rochester, New York, USA. June 17–19, 2004. pp. 273-280. ASME. https://doi.org/10.1115/ICMM2004-2345
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