Variable turbulent Prandtl number model for shock/boundary-layer interaction S Roy, U Pathak, K Sinha AIAA Journal 56 (1), 342-355, 2018 | 26 | 2018 |
Turbulent heat flux model for hypersonic shock–boundary layer interaction S Roy, K Sinha AIAA Journal 57 (8), 3624-3629, 2019 | 14 | 2019 |
Parametric study of the performance of two-dimensional scramjet intake VJ Babu, P Raje, R Singh, S Roy, K Sinha 18th Annual CFD Symposium, 1-10, 2016 | 9 | 2016 |
A phenomenological model for turbulent heat flux in high-speed flows with shock-induced flow separation U Pathak, S Roy, K Sinha Journal of Fluids Engineering 140 (5), 051203, 2018 | 6 | 2018 |
Variable turbulent Prandtl number model applied to hypersonic shock/boundary-layer interactions S Roy, K Sinha 2018 Fluid Dynamics Conference, 3728, 2018 | 5 | 2018 |
Large eddy simulation of a dual-mode scramjet with direct injection: Flame dynamics under flow separation induced by heat-release M Yuan, P Wang, Y Zhang, Y Tian, S Chen, S Roy, K Cheng Aerospace Science and Technology 139, 108401, 2023 | 2 | 2023 |
Characteristic scales in shock–turbulence interaction F Lacombe, S Roy, K Sinha, S Karl, JP Hickey AIAA Journal 59 (2), 526-532, 2021 | 2 | 2021 |
Anisotropic turbulent heat flux modelling through shock waves S Roy, K Sinha, F Lacombe, JP Hickey AIAA Aviation 2019 Forum, 3321, 2019 | 1 | 2019 |
Heat transfer prediction in shock-turbulent boundary layer interaction at flight enthalpy S Roy, B Saikia, K Sinha AIAA Scitech 2019 Forum, 0339, 2019 | | 2019 |
Variable turbulent prandtl number model for high speed flows with shock wave S Roy Mumbai, 0 | | |
Turbulent Heat Flux Model for Shock-Boundary Layer Interaction with Non-Adiabatic Wall S Roy, K Sinha | | |