EFFECT OF DIELECTRIC BARRIER DISCHARGE PLASMA ON FILM COOLING PERFORMANCE
To improve film cooling effectiveness of a gas turbine blade, a kind of plasma ac-tuator is introduced on the blade surface. The effect of three arrangements of plasma actuators on flow characteristics and film cooling performance is numer-ically investigated by a verified turbulence model. Results show that the coolant air under plasma is pulled down to the wall, and the near-wall air is sped up