| Year |
Citation |
Score |
| 2019 |
Williams DR, Greenblatt D, Müller-Vahl H, Santra S, Reißner F. Feed-Forward Dynamic Stall Control Model Aiaa Journal. 57: 608-615. DOI: 10.2514/1.J057266 |
0.313 |
|
| 2019 |
Rennie RM, Catron B, Feroz MZ, Williams D, He X. Dynamic Behavior and Gust Simulation in an Unsteady Flow Wind Tunnel Aiaa Journal. 57: 1423-1433. DOI: 10.2514/1.J057186 |
0.307 |
|
| 2018 |
Williams DR, King R. Alleviating Unsteady Aerodynamic Loads with Closed-Loop Flow Control Aiaa Journal. 56: 2194-2207. DOI: 10.2514/1.J056817 |
0.315 |
|
| 2016 |
Monnier B, Williams DR, Weier T, Albrecht T. Comparison of a separated flow response to localized and global-type disturbances Experiments in Fluids. 57. DOI: 10.1007/S00348-016-2199-4 |
0.335 |
|
| 2015 |
Albrecht T, Weier T, Gerbeth G, Monnier B, Williams DR. Separated flow response to single pulse actuation Aiaa Journal. 53: 190-199. DOI: 10.2514/1.J053026 |
0.354 |
|
| 2015 |
Choi J, Colonius T, Williams DR. Surging and plunging oscillations of an airfoil at low Reynolds number Journal of Fluid Mechanics. 763: 237-253. DOI: 10.1017/Jfm.2014.674 |
0.333 |
|
| 2015 |
Williams DR, An X, Iliev S, King R, Reißner F. Dynamic hysteresis control of lift on a pitching wing Experiments in Fluids. 56. DOI: 10.1007/S00348-015-1982-Y |
0.304 |
|
| 2014 |
Granlund K, Monnier B, Ol M, Williams D. Airfoil longitudinal gust response in separated vs. attached flows Physics of Fluids. 26. DOI: 10.1063/1.4864338 |
0.333 |
|
| 2013 |
Brunton SL, Rowley CW, Williams DR. Reduced-order unsteady aerodynamic models at low Reynolds numbers Journal of Fluid Mechanics. 724: 203-233. DOI: 10.1017/Jfm.2013.163 |
0.351 |
|
| 2011 |
Colonius T, Williams DR. Control of vortex shedding on two- and three-dimensional aerofoils. Philosophical Transactions. Series a, Mathematical, Physical, and Engineering Sciences. 369: 1525-39. PMID 21382829 DOI: 10.1098/Rsta.2010.0355 |
0.352 |
|
| 2011 |
Kerstens W, Pfeiffer J, Williams D, King R, Colonius T. Closed-Loop Control of Lift for Longitudinal Gust Suppression at Low Reynolds Numbers Aiaa Journal. 49: 1721-1728. DOI: 10.2514/1.J050954 |
0.325 |
|
| 2010 |
Taira K, Rowley CW, Colonius T, Williams DR. Lift enhancement for low-aspect-ratio wings with periodic excitation Aiaa Journal. 48: 1785-1790. DOI: 10.2514/1.J050248 |
0.341 |
|
| 2008 |
Cattafesta LN, Song Q, Williams DR, Rowley CW, Alvi FS. Active control of flow-induced cavity oscillations Progress in Aerospace Sciences. 44: 479-502. DOI: 10.1016/J.Paerosci.2008.07.002 |
0.326 |
|
| 2006 |
Rowley CW, Williams DR. Dynamics and control of high-reynolds-number flow over open cavities Annual Review of Fluid Mechanics. 38: 251-276. DOI: 10.1146/Annurev.Fluid.38.050304.092057 |
0.365 |
|
| 2006 |
Rowley CW, Williams DR, Colonius T, Murray RM, Macmynowski DG. Linear models for control of cavity flow oscillations Journal of Fluid Mechanics. 547: 317-330. DOI: 10.1017/S0022112005007299 |
0.331 |
|
| 2005 |
Kim B, Williams DR, Emo S, Acharya M. Modeling Pulsed-Blowing Systems for Flow Control Aiaa Journal. 43: 314-325. DOI: 10.2514/1.10285 |
0.33 |
|
| 2000 |
Bernhardt JE, Williams DR. Closed-Loop Control of Forebody Flow Asymmetry Journal of Aircraft. 37: 491-498. DOI: 10.2514/2.2624 |
0.308 |
|
| 1998 |
Bernhardt JE, Williams DR. Proportional Control of Asymmetric Forebody Vortices Aiaa Journal. 36: 2087-2093. DOI: 10.2514/2.310 |
0.328 |
|
| 1994 |
Mansy H, Yang P, Williams DR. Quantitative measurements of three-dimensional structures in the wake of a circular cylinder Journal of Fluid Mechanics. 270: 277-296. DOI: 10.1017/S0022112094004271 |
0.347 |
|
| 1992 |
Williams DR, Mansy H, Amato C. The response and symmetry properties of a cylinder wake subjected to localized surface excitation Journal of Fluid Mechanics. 234: 71-96. DOI: 10.1017/S0022112092000703 |
0.303 |
|
| 1989 |
Mansy H, Williams DR. Flow meter based on the trapped vortex pair fluidic oscillator Review of Scientific Instruments. 60: 935-938. DOI: 10.1063/1.1140347 |
0.302 |
|
| 1987 |
Williams DR, Economou M. Scanning laser anemometer measurements of a forced cylinder wake Physics of Fluids. 30: 2283-2285. DOI: 10.1063/1.866111 |
0.301 |
|
| 1984 |
Williams DR, Fasel H, Hama FR. Experimental determination of the three-dimensional vorticity field in the boundary-layer transition process Journal of Fluid Mechanics. 149: 179-203. DOI: 10.1017/S0022112084002603 |
0.304 |
|
| 1982 |
Horstman CC, Settles GS, Williams DR, Bogdonoff SM. REATTACHING FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOW Aiaa Journal. 20: 79-85. DOI: 10.2514/3.51049 |
0.598 |
|
| 1982 |
Settles GS, Williams DR, Baca BK, Bogdonoff SM. REATTACHMENT OF A COMPRESSIBLE TURBULENT FREE SHEAR LAYER Aiaa Journal. 20: 60-67. DOI: 10.2514/3.51047 |
0.6 |
|
| 1980 |
Williams DR, Hama FR. Streaklines in a shear layer perturbed by two waves Physics of Fluids. 23: 442-447. DOI: 10.1063/1.863012 |
0.317 |
|
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