Film cooling at hypersonic Mach numbers using forward facing array of micro-jets R Sriram, G Jagadeesh International journal of heat and mass transfer 52 (15-16), 3654-3664, 2009 | 68 | 2009 |
Shock tunnel experiments on control of shock induced large separation bubble using boundary layer bleed R Sriram, G Jagadeesh Aerospace Science and Technology 36, 87-93, 2014 | 58 | 2014 |
On the length scales of hypersonic shock-induced large separation bubbles near leading edges R Sriram, L Srinath, MKK Devaraj, G Jagadeesh Journal of Fluid Mechanics 806, 304-355, 2016 | 28 | 2016 |
Image processing techniques for shock wave detection and tracking in high speed schlieren and shadowgraph systems G Li, MB Agir, K Kontis, T Ukai, S Rengarajan Journal of Physics: Conference Series 1215 (1), 012021, 2019 | 25 | 2019 |
Correlation for length of impinging shock-induced large separation bubble at hypersonic speed R Sriram, G Jagadeesh AIAA Journal 53 (9), 2771-2776, 2015 | 21 | 2015 |
Unsteady pulsating flowfield over spiked axisymmetric forebody at hypersonic flows MI Sugarno, R Sriram, SK Karthick, G Jagadeesh Physics of Fluids 34 (1), 2022 | 14 | 2022 |
Effect of counterflow argon plasma jet on aerodynamic drag of a blunt body at hypersonic Mach numbers D Mahapatra, R Sriram, G Jagadeesh The Aeronautical Journal 112 (1137), 683-687, 2008 | 14 | 2008 |
Shock tunnel measurements of surface pressures in shock induced separated flow field using MEMS sensor array R Sriram, SN Ram, GM Hegde, MM Nayak, G Jagadeesh Measurement Science and Technology 26 (9), 095301, 2015 | 11 | 2015 |
Experimental investigations on the sharp leading-edge separation over a flat plate at zero incidence using particle image velocimetry K Fujiwara, R Sriram, K Kontis Experiments in Fluids 61, 1-21, 2020 | 10 | 2020 |
Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites CA Maddock, L Ricciardi, M West, J West, K Kontis, S Rengarajan, ... Acta Astronautica 152, 782-792, 2018 | 10 | 2018 |
Shock tunnel investigations on hypersonic impinging shock wave boundary layer interaction R Sriram | 10 | 2018 |
Vehicle and mission design of a future small payload launcher C Maddock, F Toso, L Ricciardi, A Mogavero, KH Lo, S Rengarajan, ... 21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017 | 9 | 2017 |
Experimental investigation of heat flux mitigation during Martian entry by coolant injection SM Ibrahim, R Sriram, KPJ Reddy Journal of Spacecraft and Rockets 51 (4), 1363-1368, 2014 | 9 | 2014 |
Shock-tunnel investigations on the evolution and morphology of shock-induced large separation bubbles R Sriram, G Jagadeesh The Aeronautical Journal 120 (1229), 1123-1152, 2016 | 8 | 2016 |
Control of bow shock induced three-dimensional separation using bleed through holes H Chandravamsi, S Bhardwaj, K Ramachandra, R Sriram Physics of Fluids 35 (1), 2023 | 6 | 2023 |
On the scaling of three-dimensional shock-induced separated flow due to protuberances S Bhardwaj, KHC Vamsi, R Sriram Physics of Fluids 34 (2), 076115, 2022 | 6 | 2022 |
Wake flow characteristics over an articulated lorry model with/without AC-DBD plasma actuation KH Lo, R Sriram, K Kontis Applied Sciences 9 (12), 2426, 2019 | 6 | 2019 |
How to launch small payloads? Evaluation of current and future small payload launch systems S McIntyre, T Fawcett, T Dickinson, CA Maddock, A Mogavero, L Ricciardi, ... 14th Reinventing Space Conference, 2016 | 6 | 2016 |
Density field measurements of a micro–explosion using BOS P Suriyanarayanan, N Karthikeyan, L Venkatakrishnan, O Samuelraj, ... 28th International Symposium on Shock Waves: Vol 2, 705-710, 2012 | 6 | 2012 |
Experimental investigations on the effect of a thermal bump in the hypersonic flow around a flat plate G Jagadeesh, R Sriram, MS Hariharan, S Saravanan, K Nagashetty, ... 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2009 | 6 | 2009 |