| An AMReX-based Compressible Reacting Flow Solver for High-speed Reacting Flows relevant to Hypersonic Propulsion S Sharma, R Bielawski, O Gibson, S Zhang, V Sharma, AH Rauch, ... arXiv preprint arXiv:2412.00900, 2024 | 31 | 2024 |
| Interaction of chemical reactions and turbulence in a jet in supersonic crossflow S Sharma, J Singh, L Angelilli, V Raman Proceedings of the Combustion Institute 40 (1-4), 105295, 2024 | 19 | 2024 |
| High-Fidelity Numerical Simulations of a Scramjet Flowpath AH Rauch, MJ Ullman, S Sharma, R Bielawski, V Raman, CE Dedic, ... AIAA SCITECH 2024 Forum, 2593, 2024 | 11 | 2024 |
| High-fidelity Computational Study of High-speed Reacting Jets in Crossflow S Sharma, R Bielawski, AH Rauch, V Raman AIAA SCITECH 2024 Forum, 2596, 2024 | 9 | 2024 |
| GPU Performance Modeling and Assessment of High-Speed Combustion Simulations Using Adaptive Mesh Refinement A Carreon, S Zhang, S Sharma, J Singh, V Raman AIAA SciTech 2025 Forum, 1168, 2025 | 7 | 2025 |
| Characteristic Boundary Condition for Embedded-Boundary Method Based Compressible Reacting Flow Solver S Zhang, V Sharma, S Sharma, R Bielawski, V Raman AIAA AVIATION FORUM AND ASCEND 2024, 3863, 2024 | 6 | 2024 |
| A GPU-based Compressible Combustion Solver for Applications Exhibiting Disparate Space and Time Scales A Carreon, J Singh, S Sharma, S Zhang, V Raman arXiv preprint arXiv:2510.23993, 2025 | 5 | 2025 |
| The Structure of Liquid and Gas Jets in a Supersonic Crossflow S Sharma, R Bielawski, V Raman AIAA SCITECH 2025 Forum, 1582, 2025 | 5 | 2025 |
| Shock Train Structure in Axisymmetric Domains J Singh, S Sharma, V Raman AIAA SCITECH 2024 Forum, 0113, 2024 | 3 | 2024 |
| Numerical Simulation of Reacting and Non-Reacting Liquid Jets in Supersonic Crossflow M Ullman, S Sharma, V Raman arXiv preprint arXiv:2504.15422, 2025 | 2 | 2025 |
| Aerothermodynamic design optimization of planetary vehicle S Shivank, S Harshul, NA Hammad, G Malaikannan Thermophysics and Aeromechanics 30 (3), 429-444, 2023 | 2 | 2023 |
| Droplet Identification in an Interface Capturing Volume of Fluids Approach for Liquid Jet in Supersonic Crossflow O Gibson, MJ Ullman, S Sharma, V Raman AIAA SCITECH 2026 Forum, 2185, 2026 | | 2026 |
| Effect of Injector Configuration on Flame Stabilization in Confined Supersonic Flowpaths S Sharma, J Singh, V Raman AIAA SCITECH 2026 Forum, 2910, 2026 | | 2026 |
| Interaction Between a Coaxial Rotating Jet and a Reactive Core Flow R Jain, RA Fernandez, S Sharma, YS Keskinoz, V Raman AIAA SCITECH 2026 Forum, 2188, 2026 | | 2026 |
| Impact of Varying Combustion Chamber Area in Rotating Detonation Engines M Powers, S Sharma, V Raman AIAA SCITECH 2026 Forum, 2613, 2026 | | 2026 |
| The Impact of Injected Fluid Properties on Supersonic Flow T Gautham-Pogioli, S Sharma, M Ullman, R Bielawski, V Raman AIAA AVIATION FORUM AND ASCEND 2025, 3129, 2025 | | 2025 |
| Compressibility-Turbulence-Combustion Interaction in a Scramjet Flowpath J Singh, S Sharma, V Raman AIAA SCITECH 2025 Forum, 2486, 2025 | | 2025 |
| Investigating Shock-Boundary layer Interaction via Direct Numerical Simulations J Singh, S Sharma, V Raman APS Division of Fluid Dynamics Meeting Abstracts, ZC31. 006, 2024 | | 2024 |
| Stabilization of Confined Premixed Flames in Supersonic Flows J Singh, S Sharma, V Raman Available at SSRN 5610771, 0 | | |
Venkat RamanJames Arthur Nicholls Collegiate Professor, University of MichiganVerified email at umich.edu
