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Compressible studies on dynamic stall
27th Aerospace Sciences Meeting, 1989The purpose of this work is to investigate the effects of compressibility on the dynamic stall phenomenon by numerical simulation of the unsteady flow. The full two-dimensional unsteady compressible Navier-Stokes equations are solved for flows over oscillating airfoils and airfoils pitching rapidly to high angles of attack.
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A computational study on the dynamic stall of a flapping airfoil
16th AIAA Applied Aerodynamics Conference, 1998The dynamic stall boundaries of a NACA 0012 airfoil oscillating in either the pure plunge mode or in the combined pitch and plunge mode is computed using a thin-layer Navier-Stokes solver. Unsteady flowfields are computed at the free-stream Mach number of 0.3, the Reynolds number of 1 • 10, and the Baldwin-Lomax turbulence model is employed.
Tuncer, Ismail +2 more
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Review of rotating wing dynamic stall: Experiments and flow control
Progress in Aerospace Sciences, 2023Marilyn J Smith +2 more
exaly
Numerical investigation of dynamic stall suppression of rotor airfoil via improved co-flow jet
Chinese Journal of Aeronautics, 2022Rongqian Chen, Jiaqi Liu
exaly
A method for analyzing dynamic stall
10th Aerospace Sciences Meeting, 1972P. CRIMI, B. REEVES
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The dynamic stall dilemma for vertical-axis wind turbines
Renewable Energy, 2022Sébastien le Fouest, Karen Mulleners
exaly