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  1. Numerical investigation on streamwise vortex generation by plasma actuator
  2. Numerical Analysis on Hovering Performance of Hexacopter “HAMILTON” for Mars Exploration
  3. Virtual vortex generator
  4. Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103–106
  5. Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 106