Response on the corner flow separation to plasma aerodynamic actuation in a highly loaded compressor cascade

【Author】

Yun Wu;Xiaohu Zhao;Yinghong Li;Jun Li;

【Abstract】

<正>Comer flow separation causes considerable total pressure loss and blockage in highly loaded axial compressor.Both wind-tunnel experiment and simulation are carried out to examine the effect of plasma aerodynamic actuation(PAA) on the corner flow structure and the total pressure loss.Microsecond or nanosecond pulsed PAA was used on the blade surface and the endwall.From the

【Keywords】

PAA;Response on the corner flow separation to plasma aerodynamic actuation in a highly loaded compressor cascade;

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