On vortex shedding from an airfoil in low-Reynolds-number flows

Development of coherent structures in the separated shear layer and wake of an airfoil in low-Reynolds-number flows was studied experimentally for a range of airfoil chord Reynolds numbers, 55 × 103 ≤ Rec ≤ 210 × 103, and three angles of attack, α = 0°, 5° and 10°. To illustrate the effect of separa...

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Veröffentlicht in:	Journal of fluid mechanics 2009-08, Vol.632, p.245-271
Hauptverfasser:	YARUSEVYCH, SERHIY, SULLIVAN, PIERRE E., KAWALL, JOHN G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Air flow Applied fluid mechanics Boundary layers Exact sciences and technology Flow Fluid dynamics Fluid mechanics Fundamental areas of phenomenology (including applications) Physics Reynolds number Rotational flow and vorticity Separated flows Transition to turbulence Turbulent flows, convection, and heat transfer
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