Large-eddy simulation of 3-D corner separation in a linear compressor cascade
The increase of the thrust/weight ratio of aircraft engines is extremely restricted by different 3-
D flow loss mechanisms. One of them is the corner separation that can form at the junction …
D flow loss mechanisms. One of them is the corner separation that can form at the junction …
Corner separation dynamics in a linear compressor cascade
G Zambonini, X Ottavy… - Journal of Fluids …, 2017 - asmedigitalcollection.asme.org
This paper considers the inherent unsteady behavior of the three-dimensional (3D)
separation in the corner region of a subsonic linear compressor cascade equipped of 13 …
separation in the corner region of a subsonic linear compressor cascade equipped of 13 …
Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil
M Wang, Z Li, C Yang, S Zhao, Y Zhang, X Lu - Physics of Fluids, 2020 - pubs.aip.org
A large eddy simulation (LES) was conducted to investigate the separated flow transition on
the suction surface of a high subsonic compressor airfoil at two Reynolds number (Re) …
the suction surface of a high subsonic compressor airfoil at two Reynolds number (Re) …
Modeling the wall shear stress in large-eddy simulation using graph neural networks
As the Reynolds number increases, the large-eddy simulation (LES) of complex flows
becomes increasingly intractable because near-wall turbulent structures become …
becomes increasingly intractable because near-wall turbulent structures become …
Direct numerical simulation of supersonic turbulent flows around a tandem expansion-compression corner
The M= 2.9 supersonic turbulent flows over a tandem expansion-compression corner
configuration with a sharp deflection angle of 25 at three Reynolds numbers Re δ= 20 000 …
configuration with a sharp deflection angle of 25 at three Reynolds numbers Re δ= 20 000 …
Review on the sensitization of turbulence models to rotation/curvature and the application to rotating machinery
X Huang, W Yang, Y Li, B Qiu, Q Guo… - Applied Mathematics and …, 2019 - Elsevier
The complex geometry of rotating machines makes the flows strongly affected by rotation
and curvature, which are challenging for turbulence modeling. During the development of …
and curvature, which are challenging for turbulence modeling. During the development of …
Using graph neural networks for wall modeling in compressible anisothermal flows
Compressible anisothermal flows, which are commonly found in industrial settings such as
combustion chambers and heat exchangers, are characterized by significant variations in …
combustion chambers and heat exchangers, are characterized by significant variations in …
Flow structure of a low aspect ratio wall-mounted airfoil operating in a low Reynolds number flow
Measurements on a wall-mounted NACA 0012 airfoil with an aspect ratio (AR) of 0.5
operating in the low Reynolds number (274,000, based on chord) regime were performed …
operating in the low Reynolds number (274,000, based on chord) regime were performed …
Hybrid RANS/LES simulation of corner stall in a linear compressor cascade
G Xia, G Medic, TJ Praisner - Journal of …, 2018 - asmedigitalcollection.asme.org
Current design-cycle Reynolds-averaged Navier–Stokes (RANS) based computational fluid
dynamics (CFD) methods have the tendency to over-predict corner-stall events for axial-flow …
dynamics (CFD) methods have the tendency to over-predict corner-stall events for axial-flow …
Large eddy simulation of boundary layer transition mechanisms in a gas-turbine compressor cascade
AD Scillitoe, PG Tucker… - Journal of …, 2019 - asmedigitalcollection.asme.org
Large eddy simulation (LES) is used to explore the boundary layer transition mechanisms in
two rectilinear compressor cascades. To reduce numerical dissipation, a novel locally …
two rectilinear compressor cascades. To reduce numerical dissipation, a novel locally …