| The structure of premixed particle-cloud flames K Seshadri, AL Berlad, V Tangirala Combustion and flame 89 (3-4), 333-342, 1992 | 196 | 1992 |
| Effect of heat release and swirl on the recirculation within swirl-stabilized flames V Tangirala, RH Chen, JF Driscoll Combustion science and technology 51 (1-3), 75-95, 1987 | 175 | 1987 |
| Temperatures within non-premixed flames: effects of rapid mixing due to swirl V Tangirala, JF Driscoll Combustion science and technology 60 (1-3), 143-162, 1988 | 82 | 1988 |
| High-pressure ethylene oxidation behind reflected shock waves OG Penyazkov, KL Sevrouk, V Tangirala, N Joshi Proceedings of the Combustion Institute 32 (2), 2421-2428, 2009 | 68 | 2009 |
| Turbine efficiency for unsteady, periodic flows A Suresh, DC Hofer, VE Tangirala | 64 | 2012 |
| Two-step chemical-kinetic descriptions for hydrocarbon–oxygen-diluent ignition and detonation applications B Varatharajan, M Petrova, FA Williams, V Tangirala Proceedings of the Combustion Institute 30 (2), 1869-1877, 2005 | 62 | 2005 |
| Sensitivity analysis of rotating detonation engine with a detailed reaction model AK Hayashi, Y Kimura, T Yamada, E Yamada, J Kindracki, E Dzieminska, ... 47th AIAA aerospace sciences meeting including the new horizons forum and …, 2009 | 58 | 2009 |
| System and method for controlling a pulse detonation engine ER Westervelt, ND Joshi, A Rasheed, VE Tangirala US Patent App. 12/956,868, 2012 | 54 | 2012 |
| Interactions of a pulsed detonation engine with a 2D blade cascade A Rasheed, V Tangirala, A Dean, CL Vandervort, C Haubert 42nd AIAA aerospace sciences meeting and exhibit, 1207, 2004 | 53 | 2004 |
| Compact, low pressure-drop shock-driven combustor RH Kenyon, VE Tangirala, KM Hinckley, AJ Dean, SD Myers US Patent 7,739,867, 2010 | 50 | 2010 |
| Parametric modeling approach to gas turbine combustor design VE Tangirala, AK Tolpadi, AM Danis, H Mongia Turbo Expo: Power for Land, Sea, and Air 78552, V002T02A048, 2000 | 47 | 2000 |
| System-level performance estimation of a pulse detonation based hybrid engine J Goldmeer, V Tangirala, A Dean | 43 | 2008 |
| Detonation Limit Thresholds in H2/O2 Rotating Detonation Engine T Yamada, AK Hayashi, E Yamada, N Tsuboi, VE Tangirala, T Fujiwara Combustion Science and Technology 182 (11-12), 1901-1914, 2010 | 42 | 2010 |
| Investigation of unsteady flow field in a 2-stage PDE resonator I Leyva, V Tangirala, A Dean 41st Aerospace Sciences Meeting and Exhibit, 715, 2003 | 42 | 2003 |
| Numerical analysis of threshold of limit detonation in rotating detonation engine T Yamada, K Hayashi, N Tsuboi, E Yamada, V Tangirala, T Fujiwara 48th AIAA aerospace sciences meeting including the new horizons forum and …, 2010 | 39 | 2010 |
| Pulsed detonation engine processes: Experiments and simulations VE Tangirala, AJ Dean, DM Chapin, PF Pinard, B Varatharajan Combustion science and technology 176 (10), 1779-1808, 2004 | 38 | 2004 |
| Pulse detonation engines and components thereof VE Tangirala, A Rasheed, CL Vandervort, AJ Dean US Patent 7,526,912, 2009 | 37 | 2009 |
| Experimental and numerical investigations of ejectors for PDE applications A Rasheed, P Pinard, V Tangirala, A Dean 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 4971, 2003 | 35 | 2003 |
| Dual mode combustion operation of a pulse detonation combustor in a hybrid engine VE Tangirala, A Rasheed, AJ Dean US Patent 7,950,219, 2011 | 34 | 2011 |
| Pulse detonation combustor with folded flow path DM Chapin, KM Hinckley, VE Tangirala, AJ Dean US Patent 7,966,803, 2011 | 33 | 2011 |
PenyazkovA.V. Luikov Heat and Mass Transfer Institute在 dnp.itmo.by 的电子邮件经过验证
