@inproceedings{49370ac42a0e4718a9036c3c553f9b86,
title = "Numerical investigations of synthetic jet control for TAU0015 airfoil",
abstract = "The aerodynamic performance of TAU0015 airfoil was investigated with synthetic jet control method. The simplified mathematical model of the active flow control was established with unsteady velocity boundary condition at the specific location of airfoil surface. The aerodynamic performance was simulated with synthetic jet and the efficiency of jet momentum coefficient was conducted. The result shows that the flow control model could perform the minor jet flow characteristics and higher jet momentum coefficient result better control efficiency.",
keywords = "Aerodynamics, Airfoil, Numerical simulation, Synthetic jet",
author = "Xu, {Xiao Ping} and Zhou Zhou and Rui Wang",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.598.562",
language = "英语",
isbn = "9783038351795",
series = "Applied Mechanics and Materials",
publisher = "Trans Tech Publications Ltd",
pages = "562--567",
booktitle = "Advanced Materials, Mechanics and Industrial Engineering",
note = "4th International Conference on Mechanics, Simulation and Control, ICMSC 2014 ; Conference date: 21-06-2014 Through 22-06-2014",
}