To disclose the basic mechanism of enhancing film cooling efficiency by plasma actuation produced from horseshoe plasma actuator
numerical simulation was carried out to investigate the flow field for two types of cylindrical holes with/without horseshoe plasma actuator.Results show that the jet flow has acquired expansibility by plasma actuation and the kidney-shaped vortices are changed significantly.With the pull inducement and actinic acceleration of plasma actuation
the coverage area and adherent of jet flow are improved
so the film cooling efficiency was enhanced.The film cooling efficiency of cylindrical hole with horseshoe plasma actuator is larger than that without horseshoe plasma actuator by about 165%(blowing ratio of 0.5)
148%(blowing ratio of 1.0) and 500%(blowing ratio of 1.5)
Experiment on film cooling characteristics for longitudinal corrugated heat-shield
Effect of thermal radiation on the heat transfer performance of a film cooling vane
Numerical analysis of flat plate film cooling characteristics at various streamwise angles based on plasma actuation
Influence of blowing ratio on film cooling of rotating turbine blade
Experimental study on cooling characteristics of film cooling with trapezoid tabs
Related Author
WANG Minmin
ZHAO Xi
LIN Li
王天壹
宣益民
李国占
刘华坪
陈浮
Related Institution
南京航空航天大学 能源与动力学院
哈尔滨工业大学 能源科学与工程学院
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics
Market Department of China National Aero-Technology Import and Export Corporation
College of Power and Energy Engineering, Nanjing University of Aeronautics and Astronautics