Stability and Receptivity of the Swept-Wing Boundary-Layer Flow Controlled by a Periodic Sequence of Plasma Actuators
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/S0015462821050086.pdf
Reference16 articles.
1. H. Schlichting, Boundary Layer Theory (McGraw-Hill, New York, 1968).
2. E. Moreau, “Airflow control by non-thermal plasma actuators,” J. Phys. D: Appl. Phys. 40, 605–636 (2007).
3. A. P. Kuryachii, “Control of cross flow in the three-dimensional boundary layer using space-periodic body force action,” Fluid Dynamics 44(2), 233–239 (2009).
4. S. V. Manuilovich, “Bulk forces removing the crossflow in a laminar boundary layer,” Fluid Dynamics 50(3), 387–397 (2015).
5. S. Yadala et al., “Experimental control of swept-wing transition through base-flow modification by plasma actuators,” J. Fluid Mech. 844 (2018).
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1. Resonance Impact of a Periodic Sequence of Plasma Actuators in Flow Control in a Swept-Wing Boundary Layer;Fluid Dynamics;2023-08
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