• International Journal of Technology (IJTech)
  • Vol 7, No 2 (2016)

Characteristics of Vortex Ring Formation by Synthetic Jet Actuators in Different Cavities

Characteristics of Vortex Ring Formation by Synthetic Jet Actuators in Different Cavities

Title: Characteristics of Vortex Ring Formation by Synthetic Jet Actuators in Different Cavities
Engkos A. Kosasih, Harinaldi , Ramon Trisno

Corresponding email:


Published at : 29 Feb 2016
Volume : IJtech Vol 7, No 2 (2016)
DOI : https://doi.org/10.14716/ijtech.v7i2.2986

Cite this article as:

Kosasih, E.A., Harinaldi, Trisno, R., 2016. Characteristics of Vortex Ring Formation by Synthetic Jet Actuators in Different Cavities. International Journal of Technology. Volume 7(2), pp.296-305



731
Downloads
Engkos A. Kosasih Departement of Mechanical Engineering, Faculty of Engineering, Universitas Indonesia, Kampus UI Depok, Depok 16424, Indonesia
Harinaldi Departement of Mechanical Engineering, Faculty of Engineering, Universitas Indonesia, Kampus UI Depok, Depok 16424, Indonesia
Ramon Trisno Departement of Mechanical Engineering, faculty of Engineering, University of Pancasila, Jagakarsa, Jakarta 12640, Indonesia
Email to Corresponding Author

Abstract
Characteristics of Vortex Ring Formation by Synthetic Jet Actuators in Different Cavities

This paper presents a baseline study of the development of turbulent flow separation for controlling aerodynamic phenomena, especially in the design of the vehicle body. The purpose of this study was to analyze the performance of synthetic jet actuators (SJAs) as one of the tools that can be used in reducing the flow controller separation area on the bluff body model of the vehicle. To get maximum results in the performance of the SJA, this research starts with characterizing the actuator, including changes in the shape of the cavity and orifice diameter. Cavity shapes tested were half-ball (B), tube (T) and cone (K), while orifice diameters of 3, 5 and 8 mm were examined. The study was conducted using both computational and experimental approaches. Results from both types of research methods were compared and displayed in graphical form. These results serve as a reference for determining future research. The experimental results, in the form of the flow rate for each type of cavity, determined the ability of different cavity conditions to form vortex rings, whereas in CFD simulations, the formation of vortex rings was demonstrated via the visualization of flow contours. Vortex rings occurred in cavity conditions B3, T3, T5, K3 and K5. Vortex rings were not formed on any type of cavity with an orifice having a diameter of 8 mm.

Bluff body, Reverse Ahmed body, Synthetic jet actuator, Vortex ring

References

Ahmed S.R., Ramm G., Faltin G., 1984. Some Salient Features of the Time-averaged Ground Vehicle Wake. SAE Technical Paper 840300

Bruneau, C.-H., Creusé, E., Depeyras, D., Gilliéron, P., Mortazavi, I., 2011. Active Procedures to Control the Flow Past the Ahmed Body with a 25° Rear Window. International Journal of Aerodynamics, Volume 1(3/4), pp. 299–317

Conan, B., Anthoine, J., Planquart, P., 2011. Experimental Aerodynamic Study of a Car-type Bluff Body. Experiments in Fluids, Volume 50(5), pp. 1273–1284

Fares, E., 2006. Unsteady Flow Simulation of the Ahmed Reference Body using a Lattice Boltzmann Approach. Computers & Fluids, Volume 35(8–9), pp. 940–950

Gad-el-Hak, M., 1996. Modern Development in Flow Control. Applied Mechanics Review, Volume 49(7), pp. 365–379

Glezer, A., 1988. The Formation of Vortex Rings. Physics of Fluids, Volume 31(12), pp. 3532–3542

Groupe d’experts Intergouvernemental sur l’Evolution du Climat (GIEC), 2001. Bilan 2001 Des Changements Climatiques: Les Éléments Scientifiques. Available online at: http://www.developpement-durable.gouv.fr/Rapports-d-evaluation.html, Accessed on 27 January 2015

Harinaldi, Budiarso, Tarakka R., Simanungkalit S.P., 2011. International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Volume 11(03), pp. 24–30

Hintenberger, C., Garcia-Villalba, M., Rodi, W., 2004. The Aerodynamics of Heavy Vehicles: Trucks, Buses, and Trains. Berlin: Springer

Holman, R., Utturkar, Y., Mittal, R., Smith, B.L., Cattafesta, L., 2005. Formation Criterion for Synthetic Jets. AIAA Journal, Volume 43(10), pp. 2110–2116

Hucho, W.-H., 2002. Aerodynamik der stumpfen Körper-Physikalische Grundlagen und Anwendung in der Praxis. Braunschweig: Vieweg-Verlag

Hucho, W.-H., Sorvan, G., 1993. Aerodynamics of Road Vehicles. Annual Review of Fluid Mechanics, Volume 25, pp 485–537

International Energy Agency (IEA), 2007. World Energy Outlook, China and India Insights. Paris: OECD/IEA

Kourta, A., Gilléron, P., 2009. Impact of the Automotive Aerodynamic Control on the Economic Issues. Journal of Applied Fluid Mechanics, Volume 2(2), pp. 69–75

Minguez, M., Pasquetti, R., Serre E., 2008. High-order Large Eddy Simulation of Flow over the “Ahmed Body” Car Model. Physics of Fluids, Volume 20(9), pp. 095101-1–095101-1

Rouméas, M., Gilléron, P., Kourta, A., 2009a. Analysis and Control of Near-Wake Flow over a Square-back Geometry. Computers & Fluids, Volume 38(1), pp. 60–70

Rouméas, M., Gilléron, P., Kuorta, A., 2009b. Drag Reduction by Flow Separation Control on a Car after Body. International Journal for Numerical Method in Fluids, Volume 60(11), pp. 1222–1240

Smith, B.L., Glezer, A., 1998. The Formation and Evolution of Synthetic Jets. Physics of Fluids, Volume 10(9), pp. 2281–2297

Smith, B.L., Swift, G., 2001. Synthetic Jets at Large Reynolds Number and Comparison to Continuous Jets. Postdoctoral Research. USA: American Institute of Aeronautics and Astronautics

Uruba V., Hladik O., 2009. On the Ahmed Body Wake. In: Conference Colloquium FLUID DYNAMICS, Prague

Utturkar, Y., 2002. Numerical Investigation of Synthetic Jet Flow Fields. M.S. Thesis, Department of Mechanical Engineering, University of Florida