R. Sriram
R. Sriram
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Cited by
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
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
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
Correlation for length of impinging shock-induced large separation bubble at hypersonic speed
R Sriram, G Jagadeesh
AIAA Journal 53 (9), 2771-2776, 2015
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
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
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
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
Shock tunnel investigations on hypersonic impinging shock wave boundary layer interaction
R Sriram
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
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 (9), 1-21, 2020
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
Density field measurements of a micro–explosion using BOS
P Suriyanarayanan, N Karthikeyan, L Venkatakrishnan, O Samuelraj, ...
28th International Symposium on Shock Waves, 705-710, 2012
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
Shock tunnel studies on drag reduction of a blunt body using argon plasmajet
D Mahapatra, R Sriram, G Jagadeesh
47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and …, 2009
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
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
A commercially driven design approach to UK future small payload launch systems
S McIntyre, T Fawcett, T Dickinson, M West, CA Maddock, A Mogavero, ...
14th Reinventing Space Conference, 2016
Unsteady pulsating flowfield over spiked axisymmetric forebody at hypersonic flows
MI Sugarno, R Sriram, SK Karthick, G Jagadeesh
Physics of Fluids 34 (1), 016104, 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
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