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Kshitij Sabnis
Kshitij Sabnis
Department of Engineering, University of Cambridge
Verified email at cam.ac.uk
Title
Cited by
Cited by
Year
Nozzle geometry effects on corner boundary layers in supersonic wind tunnels
K Sabnis, H Babinsky
AIAA Journal 57 (8), 3620-3623, 2019
132019
Nozzle geometry-induced vortices in supersonic wind tunnels
K Sabnis, H Babinsky, DS Galbraith, JA Benek
AIAA Journal 59 (3), 1087-1098, 2021
102021
The influence of nozzle geometry on corner flows in supersonic wind tunnels
K Sabnis, D Galbraith, H Babinsky, JA Benek
AIAA Scitech 2019 Forum, 1650, 2019
102019
Supersonic corner flows in rectangular channels
K Sabnis
52020
Flow characterisation for a validation study in high-speed aerodynamics
K Sabnis, D Galbraith, H Babinsky, JA Benek
AIAA Aviation 2019 Forum, 3073, 2019
52019
Experimental validation of the quadratic constitutive relation in supersonic streamwise corner flows
K Sabnis, D Galbraith, H Babinsky, JA Benek
AIAA Scitech 2021 Forum, 1740, 2021
42021
A review of three-dimensional shock wave–boundary-layer interactions
K Sabnis, H Babinsky
Progress in Aerospace Sciences, 100953, 2023
32023
Design of a quasi-2D rig configuration to assess nacelle aerodynamics under windmilling conditions
L Boscagli, F Tejero, AE Swarthout, DG MacManus, K Sabnis, H Babinsky, ...
AIAA Aviation 2023 Forum, 3392, 2023
32023
A wind tunnel rig to study the external fan cowl separation experienced by compact nacelles in windmilling scenarios
K Sabnis, L Boscagli, A Swarthout, F Tejero Embuena, H Babinsky, ...
AIAA Scitech 2023 Forum, 1942, 2023
32023
Effect of winglet serration geometry on the wingtip vortex
P Gehlert, K Sabnis, H Babinsky
AIAA SCITECH 2022 Forum, 1961, 2022
32022
Experimental Investigation of External Fan Cowl Separation for Compact Nacelles in Windmilling Scenarios
K Sabnis, L Boscagli, H Babinsky, DG MacManus, C Sheaf
AIAA Aviation 2023 Forum, 3394, 2023
22023
Analysis and extension of the quadratic constitutive relation for RANS methods
K Sabnis, H Babinsky, PR Spalart, DS Galbraith, JA Benek
The Aeronautical Journal 125 (1292), 1746-1767, 2021
22021
Characteristics of Shock-Induced Boundary-Layer Separation on Nacelles Under Windmilling Diversion Conditions
L Boscagli, D MacManus, F Tejero, K Sabnis, H Babinsky, CT Sheaf
AIAA Journal 62 (1), 79-91, 2024
12024
Experimental investigation of transonic external fan cowl separation
K Sabnis, L Boscagli, H Babinsky, D MacManus, CT Sheaf
Association Aeronautique Astronautique de France, 2023
12023
Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions
K Sabnis, DS Galbraith, H Babinsky, JA Benek
Experiments in Fluids 63 (12), 191, 2022
12022
Mach 3.5 Compression Corner Control Using Microvortex Generators
DC Gochenaur, RD Williams, K Sabnis, H Babinsky
AIAA Journal, 1-13, 2024
2024
Mach 3.5 Compression Corner Control Using Micro-Vortex Generators
K Sabnis, D Gochenaur, R Williams, H Babinsky
AIAA Journal, 2024
2024
Design of a New Test Rig to Investigate Transonic External Fan Cowl Separation
K Sabnis, L Boscagli, A Swarthout, H Babinsky, D MacManus, C Sheaf
2022
Experimental Investigation of Normal Shock Wave-Vortex Interactions
K Sabnis, C Warsop, H Babinsky
AIAA SCITECH 2022 Forum, 1179, 2022
2022
Lessons Learned from a Model Validation Study in High-speed Aerodynamics
K Sabnis, D Galbraith, H Babinsky, J Benek
AIAA AVIATION 2021 FORUM, 2902, 2021
2021
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