Unsteadiness of shock-boundary layer interactions in a Mach 2.0 supersonic turbine cascade

HFS Lui, TR Ricciardi, WR Wolf, J Braun, I Rahbari… - Physical Review …, 2022 - APS
The physics of shock-boundary layer interactions (SBLIs) in a supersonic turbine cascade at
Mach 2.0 and Reynolds number 395,000, based on the axial chord, is investigated through …

[PDF][PDF] Shock boundary layer interactions in supersonic turbine cascades

HFS Lui, TR Ricciardi, WR Wolf, J Braun… - ArXiv e-prints, arXiv …, 2022 - academia.edu
The physics of shock-boundary layer interactions in a supersonic turbine cascade is
investigated through a wall-resolved large eddy simulation. Special attention is given to the …

Comparison of Shock-Boundary Layer Interactions in Adiabatic and Isothermal Supersonic Turbine Cascades

H Lui, T Rodarte Ricciardi, W Wolf… - AIAA AVIATION 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-4133. vid Wall-resolved large eddy
simulations are employed to investigate the shock-boundary layer interactions (SBLIs) in a …

Comparison of Shock-Boundary Layer Interactions in Adiabatic and Isothermal Supersonic Turbine Cascades

C JUNQUEIRA-JUNIOR, WR WOLF, H FS LUI… - 2022 - sam.ensam.eu
Wall-resolved large eddy simulations are employed to investigate the shock-boundary layer
interactions (SBLIs) in a supersonic turbine cascade. An analysis of the suction side …