| Solutions of the Navier‐Stokes Equations for the Flow About a Rotor Blade BE Wake, LN Sankar Journal of the American Helicopter Society 34 (2), 13-23, 1989 | 95 | 1989 |
| Rotorcraft retreating blade stall control P Lorber, D McCormick, T Anderson, B Wake, D MacMartin, M Pollack, ... Fluids 2000 Conference and Exhibit, 2475, 2000 | 82 | 2000 |
| Solution of the unsteady Euler equations for fixed and rotor wing configurations NL Sankar, BE Wake, SG Lekoudis journal of Aircraft 23 (4), 283-289, 1986 | 74 | 1986 |
| Evaluation of a Navier‐Stokes Analysis Method for Hover Performance Prediction BE Wake, JD Baeder Journal of the American Helicopter Society 41 (1), 7-17, 1996 | 70 | 1996 |
| Investigation of high-order upwinded differencing for vortex convection BE Wake, D Choi AIAA journal 34 (2), 332-337, 1996 | 49 | 1996 |
| Streamlined bodies with counter-flow fluid injection TG Tillman, BE Wake US Patent 6,334,753, 2002 | 48 | 2002 |
| Rotor hub fairing system for a counter-rotating, coaxial rotor system FP Bertolotti, MW Scott, BE Wake, TA Egolf, DC Mccormick US Patent 7,229,251, 2007 | 45 | 2007 |
| Investigation of instabilities in a lean, premixed step combustor JM Cohen, BE Wake, D Choi Journal of Propulsion and Power 19 (1), 81-88, 2003 | 41 | 2003 |
| High-speed experiments on combustion-powered actuation for dynamic stall suppression CG Matalanis, PO Bowles, BY Min, S Jee, AE Kuczek, BE Wake, ... AIAA Journal 55 (9), 3001-3015, 2017 | 33 | 2017 |
| Combustion-powered actuation for dynamic-stall suppression: high-mach simulations and low-mach experiments CG Matalanis, BY Min, PO Bowles, S Jee, BE Wake, TM Crittenden, ... AIAA Journal 53 (8), 2151-2163, 2015 | 33 | 2015 |
| Ovate loop for rotary-wing blades TA Egolf, BE Wake US Patent 6,260,809, 2001 | 32 | 2001 |
| Experimental replication of an aeroengine combustion instability JM Cohen, JR Hibshman, W Proscia, TJ Rosfjord, BE Wake, JB McVey, ... Turbo Expo: Power for Land, Sea, and Air 78552, V002T02A013, 2000 | 31 | 2000 |
| Rotor hub fairing system for a counter-rotating, coaxial rotor system FP Bertolotti, MW Scott, BE Wake, TA Egolf, DC Mccormick, E Usta, ... US Patent 7,530,787, 2009 | 30 | 2009 |
| Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise BE Wake, TA Egolf, PF Lorber, AJ Landgrebe US Patent 5,788,191, 1998 | 30 | 1998 |
| Aerodynamic evaluation of miniature trailing-edge effectors for active rotor control CG Matalanis, BE Wake, D Opoku, BY Min, N Yeshala, L Sankar Journal of Aircraft 48 (3), 995-1004, 2011 | 29 | 2011 |
| Serrated nozzle trailing edge for exhaust noise suppression RA Reba, BE Wake, S Narayanan, T Maeder US Patent 7,543,452, 2009 | 28 | 2009 |
| Active control of multi-element rotor blade airfoils MS Torok, RC Moffitt, PF Lorber, GCR Davis, APF Bernhard, WA Welsh, ... US Patent 6,769,872, 2004 | 28 | 2004 |
| Trailing-edge flaps for rotor performance enhancement and vibration reduction K Ravichandran, I Chopra, BE Wake, B Hein Journal of the American Helicopter Society 58 (2), 1-13, 2013 | 27 | 2013 |
| Half-plow vortex generators for rotorcraft blades for reducing blade-vortex interaction noise BE Wake, PF Lorber, AJ Landgrebe US Patent 5,785,282, 1998 | 27 | 1998 |
| Hybrid actuator for helicopter rotor blade control flaps F Sun, ZA Chaudhry, JLM Yeh, MG O'callaghan, UJ Jonsson, BE Wake, ... US Patent 7,762,770, 2010 | 25 | 2010 |
