Leading-edge-vortex tailoring on unsteady airfoils using an inverse aerodynamic approach

In this paper, we present an approach to obtain a desired leading-edge vortex (LEV) shedding pattern from unsteady airfoils through the execution of suitable motion kinematics. Previous research revealed that LEV shedding is associated with the leading-edge suction parameter (LESP) exceeding a maxim...

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Veröffentlicht in:	Physics of fluids (1994) 2022-05, Vol.34 (5)
Hauptverfasser:	Suresh Babu, Arun Vishnu, Narsipur, Shreyas, Bryant, Matthew, Gopalarathnam, Ashok
Format:	Artikel
Sprache:	eng
Schlagworte:	Airfoils Algorithms Fluid dynamics Iterative methods Kinematics Leading edges Maneuvers Physics Reynolds averaged Navier-Stokes method Shedding Suction Vortices
Online-Zugang:	Volltext
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