Wind-tunnel tests of synthetic jet control effects on airfoil flow separation

To find out the comprehensive principles of synthetic jet control effects on airfoil stall characteristics, fundamental contrastive wind-tunnel tests were conducted systematically. By using six-component balance, Particle Image Velocimetry (PIV) technology and boundary layer probe, the measurements...

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Bibliographic Details
Published in:Scientific reports 2022-12, Vol.12 (1), p.21994-21994, Article 21994
Main Authors: Zhao, Guoqing, Zhao, Qijun, Chen, Xi
Format: Article
Language:English
Subjects:
639/166/984
639/766/189
Boundary layers
Flow control
Flow separation
Flow velocity
Humanities and Social Sciences
multidisciplinary
Reynolds number
Science
Science (multidisciplinary)
Velocity
Wind
Wind tunnels
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Summary:To find out the comprehensive principles of synthetic jet control effects on airfoil stall characteristics, fundamental contrastive wind-tunnel tests were conducted systematically. By using six-component balance, Particle Image Velocimetry (PIV) technology and boundary layer probe, the measurements of model aerodynamic forces, the whole velocity field over airfoil and velocity profiles in the boundary layer were conducted, respectively. Based upon the experimentally parametric analyses of synthetic jet control on airfoil, it is concluded that the incline angle of synthetic jet has an important impact on both the flow in boundary layer and aerodynamic forces of airfoil. A tangential jet inject energy and accelerate the velocity of flow in inner boundary layer thus has a better control effects on delay stall of airfoil when the momentum coefficient of jet is relatively large, and the normal jet helps to enlarge the thickness of boundary layer which is proved to have better control effects on flow separation control and improving the aerodynamic characteristics of airfoil when the momentum coefficient of a jet is relatively small.
ISSN:2045-2322
2045-2322
DOI:10.1038/s41598-022-19642-2