Numerical and Experimental Flow Analysis of Moving Airfoils with Laminar Separation Bubbles

By R. Radespiel, Jan Windte, U. Scholz. 2006

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Recent progress in flapping wing aerodynamics and aeroelasticity (2010, background): “[152] compared the flow field over a SD7003 airfoil with and without plunging motion at Re=6.”
Implicit Large Eddy Simulation of transition to turbulence at low Reynolds numbers using a Discontinuous Galerkin method (2011, methodology): “37◦ angle of attack; TU-BS [38] and HFWT [15] correspond to PIV experiments; Visbal et al.”
Shallow and deep dynamic stall for flapping low Reynolds number airfoils (2009, background): “Here, we seek to extend these results to more complex kinematics of motion, to a range of Reynolds numbers bracketing transition-dominated effects evinced in the static case and in lower-amplitude pitch–plunge cases (Radespiel et al. 2007), and to include effects of leadingedge separation.”
Stability and receptivity characteristics of a laminar separation bubble on an aerofoil (2010, methodology): “More recently, transition prediction by linear stability analysis of velocity profiles has been incorporated into unsteady Reynolds-averaged Navier–Stokes methods, for the purpose of predicting aerofoil flows (e.g. Radespiel & Scholz 2007; Yuan et al. 2007).”
Unsteady force generation and vortex dynamics of pitching and plunging aerofoils (2012, unknown): “amplitude pitching and plunging condition [86].”