Data for: A modified Leishman-Beddoes model for airfoil sections undergoing dynamic stall at low Reynolds numbers

Published: 08-01-2020| Version 1 | DOI: 10.17632/y5wt7htxdp.1
Contributors:
Johan Boutet,
Grigorios Dimitriadis,
Xavier Amandolese

Description

Comparison of experimental dynamic stall with a modified Leishman-Beddoes model. 1 ReadMe, 2 Normal force and Moment coefficient for an oscillating flat plate undergoing dynamic stall, 3 Normal force and Moment coefficient for an oscillating NACA 0012 undergoing dynamic stall 4 Normal force and Moment coefficient for an oscillating NACA 0018 undergoing dynamic stall

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