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"Airfoil Thickness Effects on Dynamic Stall Onset" by Anupam Sharma

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Berkeley Electronic Press Selected Works

Numerical Investigation of the Effect of Airfoil Thickness on Onset of ...arxiv.org › physics

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Apr 29, · Title:Numerical Investigation of the Effect of Airfoil Thickness on Onset of Dynamic Stall. Authors:Anupam Sharma, Miguel Visbal.

CiteSeerX — Flow

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BibTeX @MISC{Moarref11flow, author = {Rashad Moarref and Mihailo R. Jovanović and Binh K. Lieu and Miguel Visbal and M. Matsubara and P. H. Alfredsson}, title = {Flow}, year = {2011}}

Miguel Angel Visbal Meza - Academia.edu

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Phys. Rev. Fluids 2, (2017) - Unsteady flow structure and...

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Unsteady flow structure and loading of a pitching low-aspect-ratio wing Miguel R. Visbal Phys. Rev. Fluids 2, – Published 24 February 2017

Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low ...www.sciencegate.app › documents

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Miguel Visbal. Keyword(s):. reynolds number ◽. aspect ratio ◽. low reynolds number ◽. low aspect ratio ◽. low reynolds ◽. plasma control. Download Fulltext.

Plasma Flow Control Simulation of a Low-Reynolds Number...

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Read Plasma Flow Control Simulation of a Low-Reynolds Number Low-Aspect-Ratio Wing

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