Numerical simulation of film-cooling in two types of blade tip in rotating case is completed by SIMPLE method.Turbulent eddy viscosity is determined by k-ε two equation model
while the wall function is considered in boundary layer.The simulation shows that centrifugal and Coriolis forces affect the flow and centrifugal force also brings about buoyancy
which is different from the usual viewpoint that the rotation has no effect on heat transfer and film cooling in blade tip.The result also indicates that the cooling effectiveness of the rotating blade is better than that of non-rotating one in the range considered.
Effect of rotation on the leading-edge region film cooling of a twisted turbine blade
Effect of the second inlet location on heat transfer distribution in rotating wedgeshaped channel
Numerical investigation of flow and heat transfer characteristics in rotating square U-duct
Experimental investigation of rotating single-hole film cooling performance on suction side of a turbine blade
Numerical simulation on flow and heat transfer in rotating channel with small spacing pin-fin arrays
Related Author
陶智
马薏文
李海旺
韩枫
邓宏武
辛安
何定养
李洋
Related Institution
先进航空发动机协同创新中心
北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室
中国航空发动机集团有限公司 湖南动力机械研究所
空军勤务学院 航材管理系
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics