Modification of Spalart–Allmaras model with consideration of turbulence energy backscatter using velocity helicity
The correlation between the velocity helicity and the energy backscatter is proved in a DNS
case of 256 3-grid homogeneous isotropic decaying turbulence. The helicity is then …
case of 256 3-grid homogeneous isotropic decaying turbulence. The helicity is then …
Competing three-dimensional mechanisms in compressor flows
JV Taylor, RJ Miller - Journal of Turbomachinery, 2017 - asmedigitalcollection.asme.org
Three-dimensional design is central to all modern compressor design systems, but many of
these methods still rely on a two-dimensional and sectional view of aerodynamics at their …
these methods still rely on a two-dimensional and sectional view of aerodynamics at their …
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 …
Investigation of vortical structures and turbulence characteristics in corner separation in a linear compressor cascade using DDES
Y Liu, H Yan, L Lu, Q Li - Journal of Fluids …, 2017 - asmedigitalcollection.asme.org
Three-dimensional (3D) corner separation in a linear highly loaded compressor cascade is
studied by using delayed detached-eddy simulation (DDES) method. This paper studies the …
studied by using delayed detached-eddy simulation (DDES) method. This paper studies the …
Turbulence characteristics in corner separation in a highly loaded linear compressor cascade
H Yan, Y Liu, Q Li, L Lu - Aerospace Science and Technology, 2018 - Elsevier
The corner separation flow in a highly loaded prescribed velocity distribution (PVD) cascade
has been studied by using DDES method based on SST k–ω model (DDES-SST). The …
has been studied by using DDES method based on SST k–ω model (DDES-SST). The …
Compressor efficiency variation with rotor tip gap from vanishing to large clearance
S Sakulkaew, CS Tan… - Journal of …, 2013 - asmedigitalcollection.asme.org
Compressor efficiency variation with rotor tip gap is assessed using numerical simulations
on an embedded stage representative of that in a large industrial gas turbine with Reynolds …
on an embedded stage representative of that in a large industrial gas turbine with Reynolds …
Numerical investigations of vortex dynamics and loss generation in the corner separation region of a high subsonic compressor blade
M Wang, X Lu, S Zhao, Y Zhang - Physics of Fluids, 2023 - pubs.aip.org
Three-dimensional corner separation seriously deteriorates the aerodynamic performance
of a compressor blade. In this study, the complicated vortex dynamics and loss mechanism …
of a compressor blade. In this study, the complicated vortex dynamics and loss mechanism …
Evolution of unsteady secondary flow structures near the onset of stall in a tip-critical transonic axial flow compressor stage
The aerodynamic stability of an axial compressor stage depends on the rotor and stator.
However, due to the specific design requirements, the evolving flow field and the resulting …
However, due to the specific design requirements, the evolving flow field and the resulting …
[HTML][HTML] Numerical study of corner separation in a linear compressor cascade using various turbulence models
Y Liu, H Yan, Y Liu, L Lu, Q Li - Chinese Journal of Aeronautics, 2016 - Elsevier
Three-dimensional corner separation is a common phenomenon that significantly affects
compressor performance. Turbulence model is still a weakness for RANS method on …
compressor performance. Turbulence model is still a weakness for RANS method on …
Numerical investigation of three-dimensional separation in an axial flow compressor: the influence of freestream turbulence intensity and endwall boundary layer state
AD Scillitoe, PG Tucker… - Journal of …, 2017 - asmedigitalcollection.asme.org
Regions of three-dimensional separations are an inherent flow feature of the suction surface-
endwall corner in axial compressors. These corner separations can cause a significant total …
endwall corner in axial compressors. These corner separations can cause a significant total …