165 citations · 196 across the 7 of their papers we have counts for
7 papers
Interplay between streaks and vortices in shock-boundary layer interactions with conditional bubble events over a turbine airfoil
Hugo Lui, William Wolf
The shock-boundary layer interaction over the convex wall of a supersonic turbine vane is studied with a focus on extreme separation bubble events and the interplay between the bub…
Characterization of boundary layers on isothermal and adiabatic curved surfaces of a supersonic turbine cascade
Gabriel Y. R. Hamada, Hugo F. S. Lui, William R. Wolf +1
The effects of adiabatic and isothermal boundary conditions are investigated on the shock-boundary layer interactions (SBLIs) in a supersonic turbine cascade. Special attention is…
Characterization of supersonic boundary layers of adiabatic and isothermal curved surfaces with shock interactions
Gabriel Y. R. Hamada, William R. Wolf, Hugo F. S. Lui +1
Boundary layers of adiabatic and isothermal curved walls are investigated for a supersonic turbine cascade, including the effects of shock-boundary layer interactions (SBLIs). Wall…
A sensor-restrained artificial shear diffusivity for large-eddy simulations of vortex-dominated compressible flows
Jean Hélder Marques Ribeiro, Hugo Felippe da Silva Lui, William Roberto Wolf
We propose a sensor-restrained model for the shear viscosity term within the localized artificial diffusivity (LAD) scheme to stabilize compressible large-eddy simulations with low…
Comparison of Shock-Boundary Layer Interactions in Adiabatic and Isothermal Supersonic Turbine Cascades
H. Lui, T. R. Ricciardi, W. R. Wolf +1
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 sepa…
Unsteadiness of Shock-Boundary Layer Interactions in a Mach 2.0 Supersonic Turbine Cascade
Hugo F. S. Lui, Tulio R. Ricciardi, William R. Wolf +3
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…