| Aspects of shock wave-induced vortex breakdown IM Kalkhoran, MK Smart Progress in aerospace sciences 36 (1), 63-95, 2000 | 99 | 2000 |
| Effect of shock strength on oblique shock-wave/vortex interaction MK Smart, IM Kalkhoran AIAA journal 33 (11), 2137-2143, 1995 | 63 | 1995 |
| Measurements of supersonic wing tip vortices MK Smart, IM Kalkhoran, J Benston AIAA journal 33 (10), 1761-1768, 1995 | 54 | 1995 |
| Observation of shock wave elimination by a plasma in a Mach-2.5 flow SP Kuo, IM Kalkhoran, D Bivolaru, L Orlick Physics of Plasmas 7 (5), 1345-1348, 2000 | 53 | 2000 |
| Interaction of supersonic wing-tip vortices with a normal shock IM Kalkhoran, MK Smart, A Betti AIAA journal 34 (9), 1855-1861, 1996 | 37 | 1996 |
| Some aspects of streamwise vortex behavior during oblique shock wave/vortex interaction MK Smart, IM Kalkhoran, S Popovic Shock Waves 8, 243-255, 1998 | 32 | 1998 |
| Supersonic vortex breakdown during vortex/cylinder interaction IM Kalkhoran, MK Smart, FY Wang Journal of Fluid Mechanics 369, 351-380, 1998 | 31 | 1998 |
| Flow model for predicting normal shock wave induced vortex breakdown MK Smart, IM Kalkhoran AIAA journal 35 (10), 1589-1596, 1997 | 29 | 1997 |
| Airfoil pressure measurements during oblique shock-wave/vortex interaction in a Mach 3 stream IM Kalkhoran, PM Sforza AIAA journal 32 (4), 783-788, 1994 | 28 | 1994 |
| Vortex distortion during vortex-surface interaction in a Mach 3 stream IM Kalkhoran AIAA journal 32 (1), 123-129, 1994 | 27 | 1994 |
| Experimental study of shock-vortex interaction in a Mach 3 stream I KALKHORAN, P SFORZA, F WANG 9th applied aerodynamics conference, 3270, 1991 | 18 | 1991 |
| Jet noise reduction via fluidic injection RB Caeti, IM Kalkhoran AIAA journal 52 (1), 26-32, 2014 | 17 | 2014 |
| Numerical calibration of a conical five-hole probe for supersonic measurements IM Milanovic, IM Kalkhoran Measurement Science and Technology 11 (12), 1812, 2000 | 17 | 2000 |
| Numerical investigation of oblique shock wave/vortex interaction V Magri, IM Kalkhoran Computers & Fluids 86, 343-356, 2013 | 16 | 2013 |
| Flow field characteristics of a supersonic jet influenced by downstream microjet fluidic injection H Pourhashem, S Kumar, IM Kalkhoran Aerospace Science and Technology 93, 105281, 2019 | 15 | 2019 |
| Deflection of turbofan exhaust streams for enhanced engine/nacelle integration RH Tindell, F Marconi, I Kalkhoran, J Yetter Journal of aircraft 35 (1), 106-112, 1998 | 12 | 1998 |
| Innovative concept for cascade thrust reverser without blocker doors B Gilbert, F Marconi, I Kalkhoran, B Gilbert, F Marconi, I Kalkhoran 35th Aerospace Sciences Meeting and Exhibit, 823, 1997 | 12 | 1997 |
| Interaction of vortex with bow shock wave: Computational model, experimental validation, enhanced mixing H Pourhashem, IM Kalkhoran, S Kumar AIAA journal 56 (8), 3071-3085, 2018 | 9 | 2018 |
| Development of Polytechnic University's supersonic wind tunnel facility I KALKHORAN, R CRESCI, P SFORZA 31st Aerospace Sciences Meeting, 798, 1993 | 9 | 1993 |
| Experimental investigation of the perpendicular rotor blade-vortex interaction at transonic speeds IM Kalkhoran, DR Wilson, DD Seath AIAA journal 30 (3), 747-755, 1992 | 9 | 1992 |
Pankaj RajputAnsys Inc.Verified email at nyu.edu
Pankaj RajputAnsys Inc.Verified email at nyu.edu