| A novel long-duration hydrogen storage concept without liquefaction and high pressure suitable for onsite blending M Otto, MP Sargunaraj, A Riahi, J Kapat Turbo Expo: Power for Land, Sea, and Air 84997, V006T03A007, 2021 | 18 | 2021 |
| A study on the performance characteristics of two-stream supersonic diffusers SM Prabakar, LM Panchabudhe, TM Muruganandam, T Sundararajan Aerospace Science and Technology 95, 105470, 2019 | 14 | 2019 |
| Unsteady ground effects on a rectangular and swept wing undergoing heaving and pitching during deceleration DR Adhikari, MP Sargunaraj, CE Soto, S Bhattacharya, GE Loubimov, ... AIAA Scitech 2020 Forum, 0334, 2020 | 5 | 2020 |
| Tomographic schlieren system for visualisation of supersonic jet N Raju, M Prabakar, B Medhi, O Oliver M, TMM M. Thiruchengode 54th AIAA Aerospace Sciences Meeting, 1050, 2016 | 5 | 2016 |
| Investigation of diffusers for two stream supersonic wind tunnels M Prabakar, TMM M. Thiruchengode 54th AIAA Aerospace Sciences Meeting, 0047, 2016 | 5 | 2016 |
| Numerical Investigation of Film Cooling Effectiveness Including Shockwave Interaction in a Supersonic Nozzle Flow MP Sargunaraj, A Torres, J Garduna, M Otto, JS Kapat, S Saxena AIAA SCITECH 2022 Forum, 0795, 2022 | 3 | 2022 |
| Use of Supercritical CO2 Impingement Cooling for a Hypersonic Leading Edge MP Sargunaraj, M Otto, L Vesely, E Fernandez, JS Kapat, V Viti AIAA SCITECH 2022 Forum, 0266, 2022 | 3 | 2022 |
| Three dimensional schlieren using iterative phase tomography N Raju, MP Sargunaraj, B Medhi, M TM AIAA Scitech 2020 Forum, 2205, 2020 | 3 | 2020 |
| Experimental Investigations of a Diffuser Start/Unstart Characteristics for Two Stream Supersonic Wind Tunnel S Manoj Prabakar, TM Muruganandam 31st International Symposium on Shock Waves 2: Applications 31, 1119-1126, 2019 | 2 | 2019 |
| Effect of Mach Number on Shock Oscillations in Supersonic Diffusers SM Prabakar, C Srikanth, TM Muruganandam 30th International Symposium on Shock Waves 1: ISSW30-Volume 1, 257-261, 2017 | 2 | 2017 |
| Aerodynamics and Heat Transfer Investigation of Supercritical Carbon Dioxide Multi Jet Impingement Cooling for a Leading Edge at Hypersonic Speeds MP Sargunaraj, M Otto, L Vesely, E Fernandez, J Kapat, V Viti, S Saxena AIAA SCITECH 2023 Forum, 0389, 2023 | 1 | 2023 |
| Thermal Management Strategies for Hypersonic Flight: Supercritical CO2 Jet Impingement Cooling Investigation for Leading Edge MP Sargunaraj | | 2023 |
| The Effect of Dynamic Span Wise Bending on the Forces of a Pitching Flat Plate MP Sargunaraj | | 2021 |
| Characterization of Two Stream Diffusers and Its Effect on Flow Structure LM Panchabudhe, SM Prabakar, TM Muruganandam | | |
Muruganandam T M IITMProfessor, Aerospace engineering, IIT Madras, Chennai, India在 smail.iitm.ac.in 的电子邮件经过验证
