| FUNDAMENTALS OF TURBULENT AND MULTIPHASE COMBUSTION KK KUO, R ACHARYA | 289 | 2012 |
| Applications of Turbulent and Multiphase Combustion KK Kuo, R Acharya John Wiley & Sons, Inc., 2012 | 131 | 2012 |
| Combustion and emissions performance of low sulfur, ultra low sulfur and biodiesel blends in a DI diesel engine M Alam, J Song, R Acharya, A Boehman, K Miller SAE transactions, 1986-1997, 2004 | 122 | 2004 |
| Effect of pressure and propellant composition on graphite rocket nozzle erosion rate R Acharya, KK Kuo Journal of propulsion and power 23 (6), 1242-1254, 2007 | 111* | 2007 |
| Fuel formulation effects on diesel fuel injection, combustion, emissions and emission control A Boehman, M Alam, J Song, R Acharya, J Szybist, V Zello, K Miller The Energy Institute The Pennsylvania State University; ConocoPhillips (US), 2003 | 49 | 2003 |
| Fuel and System Interaction Effects on Urea-SCR Control of NOx in Diesel Exhaust Aftertreatment R Acharya, M Alam, A Boehman Diesel Exhaust, SP-2022, ISBN Number: 978-0-7680-1757-1, April 2006, 2006 | 27 | 2006 |
| Implementation of approximate Riemann solver to two-phase flows in mortar systems R Acharya, K Kuo | 20 | 2010 |
| Numerical simulation of graphite nozzle erosion with parametric analysis R Acharya, K Kuo 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6846, 2010 | 18 | 2010 |
| Design of a solid rocket motor for characterization of submerged nozzle erosion A Cortopassi, E Boyer, R Acharya, K Kuo 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4889, 2008 | 15 | 2008 |
| Graphite rocket nozzle erosion rate reduction by boundary-layer control using ablative materials R Acharya, K Kuo 45th AIAA Aerospace Sciences Meeting and Exhibit, 782, 2007 | 15 | 2007 |
| Finite element simulation of interior ballistic processes in 120-mm mortar system R Acharya, KK Kuo Proc. of the 23rd International Symposium on Ballistics (Tarragona, Spain …, 2007 | 11 | 2007 |
| Design and challenges of lean fully premixed injectors for gas turbine engines PP Palies, R Acharya, A Hoffie AIAA Propulsion and Energy 2019 Forum, 4257, 2019 | 10 | 2019 |
| Effect of different flash-tube vent-hole patterns on interior ballistic processes of ignition cartridge of 120-mm mortar system R Acharya International Journal of Energetic Materials and Chemical Propulsion 7 (5), 2008 | 10 | 2008 |
| Lean fully premixed injection for commercial jet engines: An initial design study P Palies, R Acharya, A Hoffie, M Thomas Turbo Expo: Power for Land, Sea, and Air 58622, V04BT04A039, 2019 | 9 | 2019 |
| Modeling and numerical simulation of interior ballistic processes in a 120mm mortar system R Acharya The Pennsylvania State University, 2009 | 9 | 2009 |
| Effect of Flash-Tube Vent-Hole Patterns on the Combustion Product Discharge Rate JD Moore, R Acharya, PJ Ferrara, KK Kuo International Journal of Energetic Materials and Chemical Propulsion 8 (3), 2009 | 9 | 2009 |
| Pyrolysis/Evaporation Study of Succinic Acid/Polyvinyl Acetate for Reducing Nozzle Throat Erosion KK Kuo, R Acharya, E Boyd, ST Thynell Journal of propulsion and power 25 (3), 801-807, 2009 | 8 | 2009 |
| Effect of reaction kinetic schemes on graphite rocket nozzle erosion rates R Acharya, KK Kuo International Journal of Energetic Materials and Chemical Propulsion 9 (1), 2010 | 7 | 2010 |
| METHOD OF CHARACTERISTICS SIMULATION OF INTERIOR BALLISTIC PROCESSES OF M1020 IGNITION CARTRIDGEIN A 120-mm MORTAR SYSTEM R Acharya, K Kuo, PJ Ferrara, JD Moore International Journal of Energetic Materials and Chemical Propulsion 6 (5), 2007 | 7 | 2007 |
| Combustion and emissions performance of low sulfur, ultra low sulfur and biodiesel blends in a DI diesel engine. SAE Paper 2004 M Alam, J Song, R Acharya, A Boehman, K Miller | 7 | 2004 |
Andre BoehmanProfessor of Mechanical Engineering, University of MichiganVerified email at umich.edu
