On the mechanism of high-incidence lift generation for steadily translating low-aspect-ratio wings
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[1] K. Mohseni,et al. Lift evaluation of a two-dimensional pitching flat plate , 2013 .
[2] T. Colonius,et al. Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers , 2009, Journal of Fluid Mechanics.
[3] Adam C. DeVoria,et al. Aspect-ratio effects on rotating wings: circulation and forces , 2015, Journal of Fluid Mechanics.
[4] M. R. Visbal,et al. Dynamics of revolving wings for various aspect ratios , 2014, Journal of Fluid Mechanics.
[5] Luis P. Bernal,et al. Unsteady aerodynamics of pitching low aspect ratio wings: A review of AVT 202 panel results (invited paper) , 2016 .
[6] Jeff D. Eldredge,et al. A Computational Study of a Canonical Pitch-Up, Pitch-Down Wing Maneuver , 2009 .
[7] Anya R. Jones,et al. Unsteady aerodynamic characteristics of a translating rigid wing at low Reynolds number , 2015 .
[8] K. Mohseni,et al. Unsteady Aerodynamics and Trailing-edge Vortex Sheet of An Airfoil , 2016 .
[9] James H. J. Buchholz,et al. Vorticity transport in the leading-edge vortex on a rotating blade , 2014, Journal of Fluid Mechanics.
[10] Miguel R. Visbal,et al. Three-dimensional vortex formation on a heaving low-aspect-ratio wing: Computations and experiments , 2013 .
[11] T. Maxworthy. Experiments on the Weis-Fogh mechanism of lift generation by insects in hovering flight. Part 1. Dynamics of the ‘fling’ , 1979, Journal of Fluid Mechanics.
[12] Wei Shyy,et al. Shallow and deep dynamic stall for flapping low Reynolds number airfoils , 2009 .
[13] K. Mohseni,et al. Vortex structure of low-aspect-ratio wings in sideslip , 2015 .
[14] T. Weis-Fogh. Quick estimates of flight fitness in hovering animals , 1973 .
[15] P. Saffman,et al. Vortex Induced Lift on Two Dimensional Low Speed Wings , 1984 .
[16] H Winter,et al. Flow phenomena on plates and airfoils of short span , 1936 .
[17] Alain Farcy,et al. Three-dimensional effects in hovering flapping flight , 2012, Journal of Fluid Mechanics.
[18] D. Rockwell,et al. Three-dimensional vortex structure on a rotating wing , 2012, Journal of Fluid Mechanics.
[19] William H. Rae,et al. Low-Speed Wind Tunnel Testing , 1966 .
[20] E. Polhamus. A concept of the vortex lift of sharp-edge delta wings based on a leading-edge-suction analogy , 1966 .
[21] S. Goldstein. Modern developments in fluid dynamics , 1938 .
[22] Wei Shyy,et al. Can Tip Vortices Enhance Lift of a Flapping Wing , 2009 .
[23] M. Koochesfahani. Vortical patterns in the wake of an oscillating airfoil , 1987 .
[24] Kamran Mohseni,et al. A Lagrangian analysis of a two-dimensional airfoil with vortex shedding , 2008 .
[25] M. Dickinson,et al. UNSTEADY AERODYNAMIC PERFORMANCE OF MODEL WINGS AT LOW REYNOLDS NUMBERS , 1993 .
[26] M. Dickinson,et al. Spanwise flow and the attachment of the leading-edge vortex on insect wings , 2001, Nature.
[27] Joseph Katz,et al. A discrete vortex method for the non-steady separated flow over an airfoil , 1981, Journal of Fluid Mechanics.
[28] M. Shields,et al. Roll Stall for Low-Aspect-Ratio Wings , 2016 .
[29] P. Saffman,et al. Prandtl–Batchelor flow past a flat plate with a forward-facing flap , 1984, Journal of Fluid Mechanics.
[30] M. Lighthill. On the Weis-Fogh mechanism of lift generation , 1973, Journal of Fluid Mechanics.
[31] Morteza Gharib,et al. Experimental study of three-dimensional vortex structures in translating and rotating plates , 2010 .
[32] Donald Rockwell,et al. Flow structure on finite-span wings due to pitch-up motion , 2011, Journal of Fluid Mechanics.
[33] A. Altman,et al. Wake Vorticity Measurements for Low Aspect Ratio Wings at Low Reynolds Number , 2007 .
[34] J. S. Sheffield,et al. Flow over a Wing with an Attached Free Vortex , 1977 .
[35] L. Lourenço. Particle Image Velocimetry , 1989 .
[36] Tang Jian,et al. Numerical and experimental study of flow structure of low-aspect-ratio wing , 2004 .
[37] Cameron Tropea,et al. Characteristic length scales for vortex detachment on plunging profiles with varying leading-edge geometry , 2014, Experiments in Fluids.
[38] H. Babinsky,et al. Lift and the leading-edge vortex , 2013, Journal of Fluid Mechanics.
[39] Kamran Mohseni,et al. Roll Stall for Low-Aspect-Ratio Wings , 2016 .
[40] T. Colonius,et al. Effect of Tip Vortices in Low-Reynolds-Number Poststall Flow Control , 2009 .
[41] Robert D. Moser,et al. Effects of Trailing-Edge Synthetic Jet Actuation on an Airfoil , 2011 .
[42] Michael V. Ol,et al. Unsteady flat plates: A cursory review of AVT-202 research (invited) , 2016 .
[43] K. Mohseni,et al. Lift Evaluation of a 2D Flapping Flat Plate , 2012, 1205.6853.
[44] C.. A CONCEPT OF THE VORTEX LIFT OF SHARP-EDGE DELTA WINGS BASED ON A LEADING-EDGE-SUCTION ANALOGY By , 2002 .
[45] Matthew Ringuette,et al. Vortex formation and saturation for low-aspect-ratio rotating flat-plate fins , 2012 .
[46] J. Hunt,et al. Kinematical studies of the flows around free or surface-mounted obstacles; applying topology to flow visualization , 1978, Journal of Fluid Mechanics.
[47] Adrian L. R. Thomas,et al. Leading-edge vortices in insect flight , 1996, Nature.
[48] G. Batchelor,et al. A proposal concerning laminar wakes behind bluff bodies at large Reynolds number , 1956, Journal of Fluid Mechanics.