journal article Mar 01, 2016

Investigation of effects of compressibility, geometric and flow parameters on the simulation of a synthetic jet behaviour

View at Publisher Save 10.1017/aer.2016.8
Abstract
ABSTRACTThe present paper focuses on a three-dimensional unsteady turbulent synthetic jet to assess the accuracy of a compressible simulation and some important parameters including the simulations of the actuator, cavity height and Reynolds number. The two-equationSST/k− ω turbulence model is used to predict the flow behaviour. Results show that the compressible simulation case is more accurate than the incompressible one and the dynamic mesh exhibits more reliable results than the mass flow inlet boundary in the compressible simulation. The compressible case displays a delay in the phase of instantaneous velocity for all three Reynolds numbers. Also, the maximum of mean velocity is less than the incompressible case. Moreover, an increase in the Reynolds number leads to an amplification of the peak of mean velocity magnitude. Finally, results demonstrate that a reduction in the cavity height regarding the compressible simulation case causes a reduction in the phase delay and rise in peak of instantaneous velocity magnitude.
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References
37
[4]
Iuso (2005)
[5]
Cain A.B. , Karl L.D. , Donovan J.F. and Smith T.D. Numerical simulation of compressible synthetic jet flow, 36th AIAA Aerospace Sciences Meeting and Exhibit, 12-15 January 1998, Reno, Nevada, US. 10.2514/6.1998-84
[11]
Rana "Dynamics of Sonic Hydrogen Jet Injection and Mixing Inside Scramjet Combustor" Eng Appl Comput Fluid Mech (2013)
[14]
Xiong "A novel optimal design for an application-oriented synthetic jet actuator" Chin J Aeronaut (2014) 10.1016/j.cja.2014.04.002
[15]
Bazdidi-Tehrani F. , Jahromi M. , Karami M. and Javadi A. Numerical analysis of a zero net mass flux jet in a quiescent medium, Proceedings of 16th Annual Conference of CFD Society Canada, University of Saskatchewan, Saskatoon, Canada, 2008.
[16]
Vukasinovic J. and Glezer A. Spot-cooling by confined, impinging synthetic jet, ASME Summer Heat Transfer Conference, 20-23 July 2003, Las Vegas, Nevada, US. 10.1115/ht2003-47245
[21]
Batikh "Numerical and experimental of micro synthetic jets for flow control" Heat Tech (2008)
[22]
Sachin "Comparison of pressure based solver with artificial compressibility method" Int J Eng Res (2014) 10.17950/ijer/v3s7/715
[24]
Numerical solution of the Navier-Stokes equations

Alexandre Joel Chorin

Mathematics of Computation 10.1090/s0025-5718-1968-0242392-2
[26]
A numerical investigation of effects of cavity and orifice parameters on the characteristics of a synthetic jet flow

Manu Jain, Bhalchandra Puranik, Amit Agrawal

Sensors and Actuators A: Physical 10.1016/j.sna.2010.11.001
[27]
Utturkar Y. , Mittal R. , Rampunggoon P. and Cattafesta L. Sensitivity of synthetic jets to the design of the cavity, 40th AIAA Aerospace Sciences Meeting and Exhibit, 14-17 January 2003, Reno, Nevada, US. 10.2514/6.2002-124
[29]
Bazdidi-Tehrani "Effects of inlet and outlet boundary conditions on the flow field of synthetic jets" Proc I Mech E Part E: J Process Mech Eng (2015)
[30]
Moran (2000)
[33]
Versteeg (2007)
[35]
Yao C. , Chen F. , Neuhart D. and Harris J. Synthetic jet flow field database for CFD validation, 2nd AIAA Flow Control Conference, 28 June–1 July 2004, Portland, Oregon, US. 10.2514/6.2004-2218
[36]
Polsenberg A. , Milano M. , Grazier M. , Fischer K. and Burdick J. Synthetic jet propulsion for small underwater vehicles, International Conference on Robotics and Automation, Barcelona, Spain, 2005.
[37]
Kordák "Novel methods for evaluation of the Reynolds number of synthetic jets" Exp Fluids (2014)
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Citations
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References
Details
Published
Mar 01, 2016
Vol/Issue
120(1225)
Pages
521-546
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Cite This Article
F. Bazdidi-Tehrani, A. Abouata, M. Hatami, et al. (2016). Investigation of effects of compressibility, geometric and flow parameters on the simulation of a synthetic jet behaviour. The Aeronautical Journal, 120(1225), 521-546. https://doi.org/10.1017/aer.2016.8
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