Formation of Shock-Wave Flow during Nanosecond Discharge Localization in Unsteady Flow in a Channel with Obstacles
Author:
Publisher
Pleiades Publishing Ltd
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1134/S0015462822601917.pdf
Reference13 articles.
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2. Wang, J.-J., Choi, K.-S., Feng, L.-H., Jukes, T.N., and Whalley, R.D., Recent developments in DBD plasma flow control, Progr. Aerosp. Sci., 2013, vol. 62, pp. 52–78. https://doi.org/10.1016/J.PAEROSCI.2013.05.003
3. Kotsonis, M., Diagnostics for characterisation of plasma actuators, Meas. Sci. Technol., 2015, vol. 26, no. 9, p. 092001. https://doi.org/10.1088/0957-0233/26/9/092001
4. Surzhikov, S.T. Hypersonic flow past sharp plate and double wedge with an electromagnetic actuator, Fluid Dyn., 2020, vol. 55, no. 6, pp. 825–839. https://doi.org/10.1134/S0015462820060117
5. Bayoda, K.D., Benard, N., and Moreau, E., Nanosecond pulsed sliding dielectric barrier discharge plasma actuator for airflow control: Electrical, optical, and mechanical characteristics, J. Appl. Phys., 2015, vol. 118, no. 6, p. 063301. https://doi.org/10.1063/1.4927844
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