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Research
  1. Queen Mary University of London
  2. Research
  3. Publications

Publications: Dr Kshitij Sabnis

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