1. J. R. Roth and Xin Dai, Optimization of the aerodynamic plasma actuator as an electrohydrodynamic (EHD) electrical device, 44th AIAA Aerospace Sciences Meeting and Exhibit, 9–12 January 2006, Reno, Nevada, AIAA 2006-1203.
2. D. V. Roupassov, I. N. Zavyalov, and A. Yu. Starikovskii, Boundary layer separation plasma control using low-temperature non-equilibrium plasma of gas discharge, 44th AIAA Aerospace Sciences Meeting and Exhibit, 9–12 January 2006, Reno, Nevada, AIAA 2006-373.
3. P. Khramtsov, O. Penyazkov, M. Chernik, I. Shatan, and I. Shikh, Effect of surface high-frequency barrier discharge on a flat plate drag reduction, 3rd Int. Workshop "Nonequilibrium Processes in Combustion and Plasma-Based Technologies," Minsk (2008), pp. 44–47.
4. G. I. Font, S. Jung, C. L. Enloe, and T. E. McLaughlin, Simulation of the effects of force and heat produced by a plasma actuator on neutral flow evolution, 44th AIAA Aerospace Sciences Meeting and Exhibit, 9–12 January 2006, Reno, Nevada, AIAA 2006-0167.
5. O. G. Penyazkov, P. P. Khramtsov, M. Yu. Chernik, I. N. Shatan, and I. A. Shikh, Influence of the plasma of a high-frequency barrier discharge on the structure of the dynamic boundary layer on a flat surface, Inzh.-Fiz. Zh., 81, No. 1, 55–61 (2008).