| Design and pitch angle optimisation of horizontal axis hydrokinetic turbine with constant tip speed ratio S Nigam, S Bansal, T Nema, V Sharma, RK Singh MATEC Web of Conferences 95, 06004, 2017 | 11 | 2017 |
| A reliable knowledge processing framework for combustion science using foundation models V Sharma, V Raman Energy and AI 16, 100365, 2024 | 1 | 2024 |
| Stabilization of Hydrogen-enriched Jet Flames in a Crossflow V Sharma, Y Tang, V Raman AIAA SCITECH 2024 Forum, 0393, 2024 | 1 | 2024 |
| 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 | | 2024 |
| Evaluation of Shock Wave-Boundary Layer Interaction Modeling Capabilities for Use in a Hypersonic Aerothermoelastic Framework E Kimmel, D Huang, V Sharma, J Singh, V Raman, PP Friedmann AIAA SCITECH 2024 Forum, 2735, 2024 | | 2024 |
| A computational study on effects of injector pitch angle on flame stabilization in opposed jets in crossflow V Sharma, Y Tang, V Raman 12th Mediterranean Combustion Symposium 2023 (12), 12, 2023 | | 2023 |
| Effects of Pitch Angle and Momentum Ratio on Flame Stabilization in Opposed Jets in Crossflow V Sharma, Y Tang, V Raman 18th International Conference on Numerical Combustion, 24, 2022 | | 2022 |
Venkat RamanProfessor, University of Michigan在 umich.edu 的电子邮件经过验证
Venkat RamanProfessor, University of Michigan在 umich.edu 的电子邮件经过验证
Yihao TangANSYS Inc, University of Michigan在 umich.edu 的电子邮件经过验证