A Hybrid Model for Lift Response to Dynamic Actuation on a Stalled Airfoil

The current research focuses on modeling the lift response due to dynamic (time-varying) “burst-type” actuation on a stalled airfoil. Here, the “burst-type” actuation refers to the synthetic jet (generated from the actuator) that is used for flow separation mitigation. Dynamic “burst-type” actuation...

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Bibliographic Details
Main Authors: Xuanhong An, David R. Williams, Maziar S. Hemati
Format: Article
Language:English
Published: MDPI AG 2020-02-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/13/4/855