Dr Kshitij Sabnis
PhD, FHEA
All Publications
2024
- Shock-induced Fan Cowl Separation during Aeroengine Windmilling at Diversion from Cruise
Sabnis K, Babinsky H, Boscagli L, MacManus D and Sheaf C
Aiaa Journal, American Institute of Aeronautics and Astronautics
13-11-2024 - Numerical and experimental investigations of diffusion-induced boundary layer separation on aero-engine nacelles
Boscagli L, Sabnis K, MacManus DG, Babinsky H, Tejero F and Sheaf C
International Journal of Heat and Fluid Flow, Elsevier vol. 109
01-10-2024 - Mach 3.5 Compression Corner Control Using Microvortex Generators
Gochenaur DC, Williams RD, Sabnis K and Babinsky H
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 62 (5), 1731-1743.
01-05-2024
2023
- Characteristics of shock-induced boundary layer separation on nacelles under windmilling diversion conditions
Boscagli L, MacManus D, Tejero F, Sabnis K, Babinsky H and Sheaf C
Aiaa Journal, American Institute of Aeronautics and Astronautics
02-11-2023 - A review of three-dimensional shock wave–boundary-layer interactions
Babinsky H and Sabnis K
Progress in Aerospace Sciences, Elsevier
24-10-2023
2022
- Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions
Sabnis K, Galbraith DS, Babinsky H and Benek JA
Experiments in Fluids, Springer Nature vol. 63 (12)
01-12-2022
2021
- Analysis and extension of the quadratic constitutive relation for RANS methods
Sabnis K, Babinsky H, Spalart PR, Galbraith DS and Benek JA
The Aeronautical Journal, Cambridge University Press (Cup) vol. 125 (1292), 1746-1767.
01-10-2021
2020
- Nozzle Geometry-Induced Vortices in Supersonic Wind Tunnels
Sabnis K, Babinsky H, Galbraith DS and Benek JA
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 59 (3), 1-12.
02-09-2020
2019
- Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
Sabnis K and Babinsky H
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 57 (8), 1-4.
12-06-2019