| Fast response co-axial thermocouple for short duration impulse facilities SLN Desikan, K Suresh, K Srinivasan, PG Raveendran Applied Thermal Engineering 96, 48-56, 2016 | 43 | 2016 |
| Strut-based gaseous injection into a supersonic stream SLN Desikan, J Kurian Journal of propulsion and power 22 (2), 474-477, 2006 | 32 | 2006 |
| Experimental investigation of starting characteristics and wave propagation from a shallow open cavity and its acoustic emission at supersonic speed S Pandian, SLN Desikan, S Niranjan Physics of Fluids 30 (1), 2018 | 26 | 2018 |
| Isolator characteristics under steady and oscillatory back pressures R Saravanan, SLN Desikan, M TM Physics of Fluids 32 (9), 096104, 2020 | 23 | 2020 |
| Experimental investigation of start/unstart process during hypersonic intake at Mach 6 and its control R Saravanan, SLN Desikan, KJ Francise, R Kalimuthu Aerospace Science and Technology 113, 106688, 2021 | 21 | 2021 |
| Fore-body and base heat flux measurements on a typical crew module in short duration impulse facilities K Srinivasan, SLN Desikan, R Saravanan, A Kumar, PK Maurya Applied Thermal Engineering 103, 842-854, 2016 | 19 | 2016 |
| Mixing studies in supersonic flow employing strut based hypermixers SLN Desikan, J Kurian 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3643, 2005 | 19 | 2005 |
| Experiments on atomization and spray characteristics of an effervescent strut injector M Chakraborty, A Vaidyanathan, SLN Desikan Physics of Fluids 33 (1), 2021 | 14 | 2021 |
| Supersonic combustion of a scramjet engine using hydrogen fuel in shock tunnel K Srinivasan, PK Maurya, K Abhishek, SLN Desikan, B Murugan AIAA Journal 56 (9), 3600-3609, 2018 | 14 | 2018 |
| Investigation of Supersonic Jet Interaction with Hypersonic Cross Flow D SLN, SSP R. Saravanan, S. Subramanianm AE ASME Journal of Fluid engineering 137 ((10) :101101-1011), 2015 | 13* | 2015 |
| Nonlinear characteristics of a rectangular cavity in supersonic flow S Pandian, SLN Desikan, S Niranjan AIAA Journal 58 (3), 1206-1215, 2020 | 12 | 2020 |
| Effect of back pressure and freestream dynamic pressure on a typical Ramjet engine duct under realistic supersonic inlet condition SLNDTMM R. Saravanan The Aeronautical Journal 122 (1247), 83-103, 2018 | 10 | 2018 |
| Effect of freestream–plume interaction on launch vehicle aerodynamics SLN Desikan, K Suresh, R Saravanan, MM Patil, P Balasubramanian, ... Journal of Spacecraft and Rockets 53 (2), 354-369, 2016 | 10 | 2016 |
| Twin jet interaction and reverse flow SLN Desikan, B Murugan, K Srinivasan, S Sajan Journal of Spacecraft and Rockets 52 (6), 1577-1585, 2015 | 10 | 2015 |
| Effect of cavity rear wall modifications on pressure fluctuations at supersonic speed TV Krishna, P Kumar, S Das, SLN Desikan Acta Astronautica 185, 78-88, 2021 | 9 | 2021 |
| Onset of cavity oscillation from transverse to longitudinal mode in a supersonic flow S Pandian, SLN Desikan, S Niranjan Journal of Fluids Engineering 142 (6), 061203, 2020 | 9 | 2020 |
| Understanding of flow features over a typical crew module at Mach 4 SLN Desikan, MM Patil, S Subramanian The Aeronautical Journal 119 (1216), 727-746, 2015 | 9 | 2015 |
| Transient characteristics of a typical vacuum ejector—An experimental study M Raju, SLN Desikan, A Vaidyanathan Physics of Fluids 34 (9), 2022 | 8 | 2022 |
| Experiments on flow past cavity and the application of modal decomposition techniques SLN Desikan, S Pandian, PP Simha, N Sahoo European Journal of Mechanics-B/Fluids 94, 293-298, 2022 | 8 | 2022 |
| Numerical investigation of the role of hyper-mixers in supersonic mixing SLN Desikan, K Kumaran, V Babu The Aeronautical Journal 114 (1161), 659-672, 2010 | 8 | 2010 |
