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Frequency Effects on the Aerodynamic Mechanisms of a Heaving Airfoil in a Forward Flight Configuration by Jean-Yves Andro; Laurent Jacquin is a Engineering article available to read on EtoBox.

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We present 2D direct numerical simulations of a heaving airfoil NACA 0012 at Re = 1000. We analyze the three fundamental mechanisms that govern aerodynamic efforts acting on the airfoil and which are: (i) suction by the leading edge vortex, (ii) added mass reaction and (iii) "wake capture". We decouple these different mechanisms and compare their relative strength when we increase the frequency. We first show that the contribution of the leading edge vortex, which forms and detaches on a time scale fixed by a global hydrodynamic instability, can be described by means of a quasi steady analysis at low enough frequencies. Then we emphasize that the added mass reaction, which is the counter reaction of the fluid displaced with the wing, becomes comparable to circulatory forces at high enough frequencies. Finally, the "wake capture", which concerns interactions between the airfoil and the depression regions related to previous stroke vortices, is shown to depend greatly on frequency and we also show that its contribution to the lift becomes large for particular frequencies. Finally, comparing the relative amplitudes and the interactions of these three mechanisms, we propose the followi

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Author

Jean-Yves Andro; Laurent Jacquin

Publisher

Elsevier Science; Elsevier ; Elsevier BV (ISSN 1270-9638)

Published

2009

Language

EN

Field

Engineering (Physical Sciences)