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Subhajit Roy
Subhajit Roy
Doctoral student, Department of Aerospace Engg., IIT Bombay
Verified email at iitb.ac.in
Title
Cited by
Cited by
Year
Variable turbulent Prandtl number model for shock/boundary-layer interaction
S Roy, U Pathak, K Sinha
AIAA Journal 56 (1), 342-355, 2018
262018
Turbulent heat flux model for hypersonic shock–boundary layer interaction
S Roy, K Sinha
AIAA Journal 57 (8), 3624-3629, 2019
142019
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
92016
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
62018
Variable turbulent Prandtl number model applied to hypersonic shock/boundary-layer interactions
S Roy, K Sinha
2018 Fluid Dynamics Conference, 3728, 2018
52018
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
22023
Characteristic scales in shock–turbulence interaction
F Lacombe, S Roy, K Sinha, S Karl, JP Hickey
AIAA Journal 59 (2), 526-532, 2021
22021
Anisotropic turbulent heat flux modelling through shock waves
S Roy, K Sinha, F Lacombe, JP Hickey
AIAA Aviation 2019 Forum, 3321, 2019
12019
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
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