Numerical Investigations of Synthetic Jet Control for TAU0015 Airfoil

Xiao Ping Xu; Zhou Zhou; Rui Wang

doi:10.4028/www.scientific.net/AMM.598.562

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 598Numerical Investigations of Synthetic Jet Control...

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.

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Periodical:

Applied Mechanics and Materials (Volume 598)

Pages:

562-567

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.598.562

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Online since:

July 2014

Authors:

Xiao Ping Xu*, Zhou Zhou, Rui Wang

Keywords:

Aerodynamic, Airfoil, Numerical Simulation, Synthetic Jet

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