采用商业软件ANSYSCFX研究了具有圆形和椭圆形柯恩达表面的环量控制叶型在不同射流速度下的流场和性能。结果表明：小的射流速度和大的柯恩达表面型线曲率是导致射流分离的主要因素，采用高速射流绕流大曲率柯恩达表面能够获得较大气流角和膨胀比，但同时带来较大的能量损失，叶栅气动性能与柯恩达表面形状和射流条件密切相关。
The idea of application of Coanda effect to gas turbine was proposed and studied in the paper. The performance of circulation control cascade with different Coanda surfaces was obtained through 2-D numerical simulation. The results show that high-speed jet flowing over the Coanda surface with a large curvature brings a high flow angle and expansion ratio as well as a high energy loss. Jet detachment occurs when a low-speed jet flows around the Coanda surface with a large curvature. The aerodynamic performance of the cascade is closely related to the Coanda surface shape and the jet condition.
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