Physical analysis of the coherent motion during hysteretic static stall of Naca foil using proper orthogonal decomposition
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en
Communication dans un congrès avec actes
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Second International conference on high Reynolds number vortex interactions, 2009-08-31, Brest.
Resumen en inglés
At static stall of airfoil, an hysteretic behavior (corresponding to an abrupt loss of lift) has been observed leading to a partially detached flow (called state I, upper increasing angle branch) and massively separated ...Leer más >