Hostname: page-component-8448b6f56d-xtgtn Total loading time: 0 Render date: 2024-04-19T23:43:10.719Z Has data issue: false hasContentIssue false
  • English
  • Français

Analytical Model: Characteristics of Nanosecond Pulsed Plasma Synthetic Jet Actuator in Multiple-Pulsed Mode

Part of: Compressible fluids and gas dynamics, general Ionized gas flow in electromagnetic fields; plasmic flow Applications to specific types of physical systems Shock waves and blast waves Systems theory and control: General

Published online by Cambridge University Press:  09 January 2017

Zheng Li ,
Zhiwei Shi  and
Hai Du
Zheng Li
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Zhiwei Shi*
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Hai Du
Affiliation:
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
*
*Corresponding author. Email:szwam@nuaa.edu.cn (Z. W. Shi)
Get access

Abstract

Multi-field coupling simulation method based on the physical principles is used to simulate the discharge characteristics of nanosecond pulsed plasma synthetic jet actuator. Considering the effect of the energy transferring for air, the flow characteristics of nanosecond pulsed plasma synthetic jet actuator are simulated. The elastic heating sources and ion joule heating sources are the two main sources of energy. Through the collisions, the energy of ions is transferred to the neutral gas quickly. The flow characteristics of a series of blast waves and the synthetic jet which erupt from the plasma synthetic jet (PSJ) actuator are simulated. The blast wave not only promotes outward, but also accelerates the gas mixing the inhaled gas from the outside cavity with the residual gas inside the cavity. The performances of PSJ actuator fluctuate in the first three incentive cycles and become stable after that.

Keywords

PSJ actuatordischargesingle-pulsedmultiple-pulsedblast wavejet

MSC classification

Secondary: 93A30: Mathematical modeling (models of systems, model-matching, etc.) 76L05: Shock waves and blast waves 76N25: Flow control and optimization 76X05: Ionized gas flow in electromagnetic fields; plasmic flow 82D10: Plasmas
Type
Research Article
Information
Advances in Applied Mathematics and Mechanics , Volume 9 , Issue 2 , April 2017 , pp. 439 - 462
Copyright
Copyright © Global-Science Press 2017 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

[1] Smith, B. L. and Glezer, A., Vectoring and small-scale motions effected in free shear flows using synthetic jet actuators, AIAA Aerospace Sciences Meeting & Exhibit, 35th, Reno, NV, January 6-9, (1997), AIAA Paper 97-0213.Google Scholar
[2] Corke, T. C. and Post, M. L., Overview of plasma flow control: concepts, optimization, and applications, The 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January, (2005), AIAA Paper 2005-563.Google Scholar
[3] Linda, D. K., Active flow control technology, ASME Fluids Engineering Division Technical Brief, 1998 (1998).Google Scholar
[4] Sahoo, D., Annaswamy, A. and Alvi, F., Active store trajectory control in supersonic cavities using microjets and low-order modeling, AIAA J., 45(3) (2007).CrossRefGoogle Scholar
[5] Kumar, V. and Farrukh, A., Efficient control of separation using microjets, The 35th AIAA Fluid Dynamics Conference and Exhibit, 6-9 June, (2005), Toronto, Ontario, Canada, AIAA Paper 2005-4879.Google Scholar
[6] Ali, M., Solomon, J., Gustavsson, J., Kumar, R. and Alvi, F., Control of resonant flow inside a supersonic cavity using high bandwidth pulsed micro-actuators, The 48th Aerospace Sciences Meeting, Orlando, FL, January, (2010).Google Scholar
[7] Samimy, M., Adamovich, I., Kim, J. H., Webb, B., Keshav, S. and Utkin, Y., Active control of high speed jets using localized arc filament plasma actuators, The 2nd AIAA Flow Control Conference, Portland, OR, June, (2004).Google Scholar
[8] Adamovich, I. V., Choi, I. and Jiang, N. et al., Plasma assisted ignition and high-speed flow control, Non-thermal and thermal effects, Plasma Sources Sci. Technol., 18 (2009), 034018.Google Scholar
[9] Kleinman, R. R., Bodony, D. J. and Freund, J. B., Shear-flow excitation mechanisms of recessed localized arc-filament plasma actuators, Phys. Fluids, 22 (2010), 116103.Google Scholar
[10] Lazar, E., Elliott, G. and Glumac, N., Energy deposition applied to a transverse jet in a supersonic crossflow, AIAA J., 48(8) (2010), pp. 1662–1672.Google Scholar
[11] Sinha, A., Alkandry, H. and Kearney-Fischer, M. et al., The impulse response of a high-speed jet forced with localized arc filament plasma actuators, Phys. Fluids, 24 (2012), 125104.Google Scholar
[12] Webb, N., Clifford, C. and Samimy, M., Control of oblique shock wave/boundary layer interactions using plasma actuators, Exp. Fluids, 54(6) (2013), 1545.CrossRefGoogle Scholar
[13] Cybyk, B. Z., Grossman, K. R. and Vanwie, D. M., Computational assessment of the spark jet flow control actuator, The 33rd AIAA Fluid Dynamics Conference and Exhibit, 23-26 June, (2003), Orlando, Florida, USA. AIAA paper 2003-3711.Google Scholar
[14] Cybyk, B. Z., Grossman, K. R. and Wilkerson, J. T., Performance characteristics of the spark jet flow control actuator, The 2nd AIAA Flow Control Conference, 28 June-1 July, Portland, Oregon, USA, AIAA paper 2004-2131 (2004).Google Scholar
[15] Cybyk, B. Z., Grossman, K. R. and Wilkerson, J. T. et al., Single-pulse performance of the sparkjet flow control actuator, The 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January, (2005), Reno, Nevada, USA, AIAA paper 2005-401.CrossRefGoogle Scholar
[16] Cybyk, B. Z., Grossman, K. R., Wilkerson, J. T., Chen, J. and Katz, J., Experimental characterization of a supersonic flow control actuator, The 43rd AIAA Aerospace Science Meeting and Exhibit, 10-13 January, (2005), Reno, Nevada, USA, AIAA paper 2005-401.Google Scholar
[17] Cattafesta, L. N. and Sheplak, M., Actuators for active flow control, Annu. Rev. Fluid Mech., 43 (2011), pp. 247–272.Google Scholar
[18] Grossman, K. R., Cybyk, B. Z. and Vanwie, D. M., Sparkjet actuators for flow control, The 41st AIAA Aerospace Sciences Meeting and Exhibit, 6-9 January, (2003), Reno, Nevada, USA, AIAA paper 2003-57.Google Scholar
[19] Haack, Sarah J., Bruce Land, H. and Cybyk, Bohdan et al., Characterization of a high-speed flow control actuator using digital speckle tomography and PIV, The 4th Flow Control Conference, 23-26 June, (2008), Seattle, Washington, USA, AIAA paper 2008-3759.CrossRefGoogle Scholar
[20] Haack, Sarah J., Taylor, Trent, Emhoff, Jerry and Cybyk, Bohdan, Development of an analytical sparkjet model, The 5th Flow Control Conference, 28 June-1 July, (2010), Chicago, Illinois, USA, AIAA paper 2010-4979.CrossRefGoogle Scholar
[21] Grossman, K. R., Cybyk, B. Z. and Vanwie, D. M., Characterization of sparkjet actuators for flow control, The 41st Aerospace Science Meeting and Exhibit, 5-8 January, (2004), Reno Nevada, USA, AIAA paper 2004-89.Google Scholar
[22] Anderson, Kellie V. and Knight, Doyle D., Plasma jet for flight control, AIAA J., 50(9) (2012), pp. 1855–1872.CrossRefGoogle Scholar
[23] Caruana, D., Barricau, P. and Hardy, P. et al., The “Plasma Synthetic Jet” actuator, aerothermodynamic characterization and first flow control applications, The 47th AIAA Aerospace Sciences Meeting Inculding the New Horizons Forum and Aerospace Exposition, 5-8 January, (2009), Orlando Florida, USA, AIAA paper 2009-1307.Google Scholar
[24] Kossyi, A.,Kostinsky, A. Yu., Matveyev, A. A. and Silakov, V. P., Kinetic scheme of the non-equilibrium discharge in nitrogen-oxygen mixtures, Plasma Sources Science and Technology, 1(3) (1992), pp. 207–220.Google Scholar
[25] Breden, Doug and Raja, Laxminarayan, Simulations of nanosecond pulse plasmas in supersonic flows for combustion applications, AIAA J., 50(2) (2012), pp. 647–658.Google Scholar
[26] Adamovich, Igor V., Little, Jesse and Nishihara, Munetake et al., Nanosecond pulse surface discharges for high-speed flow control, The 6th AIAA Flow Control Conference, 25-28 June, (2012), New Orleans, Louisiana, USA, AIAA paper 2012-3137.CrossRefGoogle Scholar