Dr Kshitij Sabnis
PhD, FHEA
All Publications
2025
- Shock-Induced Fan Cowl Separation During Aeroengine Windmilling at Diversion from Cruise
Sabnis K, Babinsky H, Boscagli L
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 63 (3), 825-838.
01-03-2025
2024
- Numerical and experimental investigations of diffusion-induced boundary layer separation on aero-engine nacelles
Boscagli L, Sabnis K, MacManus DG, Babinsky H
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
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 62 (5), 1731-1743.
01-05-2024 - Characteristics of Shock-Induced Boundary-Layer Separation on Nacelles Under Windmilling Diversion Conditions
Boscagli L, MacManus D, Tejero F, Sabnis K
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 62 (1), 79-91.
01-01-2024
2023
- A review of three-dimensional shock wave–boundary-layer interactions
Sabnis K
Progress in Aerospace Sciences, Elsevier vol. 143
01-11-2023
2022
- Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions
Sabnis K, Babinsky H
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
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, 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, Babinsky H
Aiaa Journal, American Institute of Aeronautics and Astronautics (Aiaa) vol. 57 (8), 1-4.
12-06-2019