Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers

By Kunihiko Taira, Tim Colonius. Journal of Fluid Mechanics, 2009

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Flow-induced vibrations of low aspect ratio rectangular membrane wings (2011, background): “Taira and Colonius (2009) reported the modified Strouhal number to be 0.”
Modal Analysis of Fluid Flows: An Overview (2017, background): “1 Modal decomposition of two-dimensional incompressible flow over a flat-plate wing [25,26] (Re 100 and α 30 deg).”
Recent progress in flapping wing aerodynamics and aeroelasticity (2010, methodology): “Taira and Colonius [83] utilized the immersed boundary method (IBM) to highlight the 3-D separated flow and vortex dynamics for a number of low aspect ratio flat plates at different angles of attacks.”
Reynolds number and aspect ratio effects on the leading-edge vortex for rotating insect wing planforms (2013, background): “Studies that have investigated 2D and 3D translating wings at insect Reynolds numbers and high angles of attack have shown that the LEV is shed after a few chord lengths of travel (Dickinson & Gotz 1993; Miller & Peskin 2004; Taira & Colonius 2009).”