Modification of Spalart–Allmaras model with consideration of turbulence energy backscatter using velocity helicity

Y Liu, L Lu, L Fang, F Gao - Physics Letters A, 2011 - Elsevier
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 …

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 …

Large-eddy simulation of 3-D corner separation in a linear compressor cascade

F Gao, W Ma, G Zambonini, J Boudet, X Ottavy, L Lu… - Physics of …, 2015 - pubs.aip.org
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 …

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 …

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 …

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 …

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 …

Evolution of unsteady secondary flow structures near the onset of stall in a tip-critical transonic axial flow compressor stage

L Kumar, DB Alone, AM Pradeep - Physics of Fluids, 2023 - pubs.aip.org
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 …

[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 …

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 …