Experimental Investigation on the Impact of Distorted Signal on Synthetic Jet

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Effective techniques for cooling electronic devices must deal with increasing heat loads associated with higher heat flux density. Many conventional cooling techniques like fan are reaching the limits of their effectiveness and shape. The novel method of heat transfer enhancement is synthetic jet. In this paper experimental results are presented. Synthetic jet actuator consist of STX 6.5 inch speaker installed in metacrylate chamber with circular orifice. The actuator was powered with signal from amplifier. The signal consist of basic sinusoidal function and THD noise added with some amplitude. The root mean square of signal voltage was constant 4V. The properties of synthetic jet were measured using constant temperature thermo-anemometer. Instantaneous velocity of air was measured in the orifice center and compared with input signal. Additional RMS and average velocity of air were measured. Measurement revealed that input signal of synthetic jet generator can contain some noise without effect on RMS and average velocity of air in the orifice. The THD less than 1% does not cause negative effect on synthetic jet fluid velocity.

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104-111

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April 2016

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© 2016 Trans Tech Publications Ltd. All Rights Reserved

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[1] J. Campbell, W. Black, & A. Glezer, (1998), Thermal management of a laptop computer with synthetic air microjets, in InterSociety Conference on Thermal Phenomena, IEEE, p.43–50.

DOI: 10.1109/itherm.1998.689518

Google Scholar

[2] M. Chaudhari, B. Puranik, A, Agrawal: Heat transfer characteristic of synthetic jet impingement cooling, International Journal of Heat and Mass Transfer 53 (2010) s. 1057-1069.

DOI: 10.1016/j.ijheatmasstransfer.2009.11.005

Google Scholar

[3] M. Chaudhari, G. Verma, B. Puranik, A. Agrawal.: Effect of orifice shape in synthetic jet based impingement cooling, Experimental Thermal and Fluid Science 34 (2010) 246-256.

DOI: 10.1016/j.expthermflusci.2009.11.001

Google Scholar

[4] Q. Gallas: On the modeling and design of zero-net mass flux actuator. Doctor of Philosophy dissertation. The University of Florida (2005).

Google Scholar

[5] P. Gil, R. Smusz, P. Strzelczyk: Badania eksperymentalne wymiany ciepła przy wykorzystaniu strugi syntetycznej. Praca zbiorowa pod red. Smusz: Termodynamika i wymiana ciepła w badaniach procesów cieplno-przepływowych. Rzeszów 2014 s. 187-198.

Google Scholar

[6] R.J. Holman: An experimental investigation of flow from zero-net mass-flux actuator. Doctor of Philosophy dissertation. The University of Florida (2006).

Google Scholar

[7] A.J. C King, D. Jagannatha: Simulation of synthetic jets with non-sinusoidal forcing functions for heat transfer applications. 18th Word IMACS/MODSIM Congress, Cairns, Australia (2009).

Google Scholar

[8] R. Mahalingam & A. Glezer (2002), Air cooled heat sinks integrated with synthetic jets, in Proc. IEEE InterSociety Conference on Thermal Phenomena, IEEE, p.285–291.

DOI: 10.1109/itherm.2002.1012469

Google Scholar

[9] R. Mahalingam & N. Rumigny (2004), Thermal management using synthetic jet ejectors, IEEE 27(3), 439–444.

DOI: 10.1109/tcapt.2004.831757

Google Scholar

[10] A. Pavlova, M. Amitay: Electronic cooling with synthetic jet impingement, Journal of Heat Transfer 128 (2006) 897–907.

DOI: 10.1115/1.2241889

Google Scholar

[11] B.L. Smith & G. Swift (2003), A comparison between synthetic and continuous jets, Experiments in Fluids 34, 467–472.

DOI: 10.1007/s00348-002-0577-6

Google Scholar

[12] Y. Utturkar, R. Holman (2005): Formation criterion for synthetic jets, AIAA 43(10), 2110–2116.

DOI: 10.2514/1.12033

Google Scholar