柯恩达表面形状对燃机涡轮环量控制叶型性能影响
Performance of Circulation Control Gas Turbine Blades with Different Coanda Surfaces
采用商业软件ANSYS CFX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。
his paper presents the results of a two-dimensional numerical research using commercial software ANSYS CFX on the performance and flow field of circulation control turbine blades with circular and elliptical Coanda surfaces. The results indicate that the jet detachment is largely due to the low magnitude of jet velocity and the great curvature of Coanda surface. A large turning of the mainstream along with a high energy loss can be obtained by a high speed jet flowing around Coanda surface with a large curvature.
李亚超、陈浮、宋彦萍
热力工程、热机
燃机涡轮环量控制叶型柯恩达表面形状射流速度
Gas turbineirculation control turbine bladesoanda surfaceJet speed
李亚超,陈浮,宋彦萍.柯恩达表面形状对燃机涡轮环量控制叶型性能影响[EB/OL].(2010-03-26)[2025-08-16].http://www.paper.edu.cn/releasepaper/content/201003-900.点此复制
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