Initial acceleration effects on the flow field development around rapidly pitching airfoils

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Publisher website

11 January 1993

conference paper
Published by American Institute of Aeronautics and Astronautics (AIAA)

DOI:10.2514/6.1993-438

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

On the formation and control of the dynamic stall vortex on a pitching airfoil
1991
Investigation of the flow structure around a rapidly pitching airfoil
AIAA Journal, 1989