Preconditioned multigrid methods for unsteady incompressible flows
C Liu, X Zheng, CH Sung - Journal of Computational physics, 1998 - Elsevier
A highly efficient numerical approach based on multigrid and preconditioning methods is
developed for modeling 3D steady and time-dependent incompressible flows. Thek-ω …
developed for modeling 3D steady and time-dependent incompressible flows. Thek-ω …
A Strongly Coupled Time-Marching Method for Solving the Navier–Stokes andk-ω Turbulence Model Equations with Multigrid
F Liu, X Zheng - Journal of Computational Physics, 1996 - Elsevier
Many researchers use a time-lagged or loosely coupled approach in solving the Navier–
Stokes equations and two-equation turbulence model equations in a time-marching method …
Stokes equations and two-equation turbulence model equations in a time-marching method …
Turbulent transition simulation using the k–ω model
This paper describes a novel approach in simulating laminar to turbulent transition by using
two‐equation models. The Total Stresses Limitation (TSL) concept is used to make the two …
two‐equation models. The Total Stresses Limitation (TSL) concept is used to make the two …
Experimental investigations on common research model at ONERA-S1MA–Drag prediction workshop numerical results
A Cartieri, D Hue, Q Chanzy, O Atinault - Journal of Aircraft, 2018 - arc.aiaa.org
This paper aims to present some of the experimental and numerical results obtained with the
NASA–Boeing Common Research Model at ONERA. The wind tunnel model used in the …
NASA–Boeing Common Research Model at ONERA. The wind tunnel model used in the …
[HTML][HTML] Application of immersed boundary method in turbomachines
C Congcong, W Yuwei, W Zhuo, DU Lin… - Chinese Journal of …, 2023 - Elsevier
Simulating unsteady turbulent flow in turbomachines is still challenging due to the
complexity of blade geometry and relative motion between rotor and stator. This study …
complexity of blade geometry and relative motion between rotor and stator. This study …
Assessment of Reynolds-Averaged Navier–Stokes/Blade Element Theory Body Force Method for Propeller Modeling
H Pantel, F Falissard, G Dufour - AIAA Journal, 2024 - arc.aiaa.org
This work presents an actuator disk-like body force method designed for propeller modeling,
which is based on a full coupling between computational fluid dynamics (CFD) and blade …
which is based on a full coupling between computational fluid dynamics (CFD) and blade …
Influence of torque ratio on counter-rotating open-rotor interaction noise
G Delattre, F Falissard - AIAA Journal, 2015 - arc.aiaa.org
This paper investigates the influence of the torque ratio, at constant total thrust, on the
interaction noise of a generic counter-rotating open rotor in pusher configuration. It is shown …
interaction noise of a generic counter-rotating open rotor in pusher configuration. It is shown …
Steady/unsteady reynolds-averaged navier–stokes and large eddy simulations of a turbine blade at high subsonic outlet mach number
T Léonard, LYM Gicquel… - Journal of …, 2015 - asmedigitalcollection.asme.org
Reynolds-averaged Navier–Stokes (RANS), unsteady RANS (URANS), and large eddy
simulation (LES) numerical approaches are clear candidates for the understanding of …
simulation (LES) numerical approaches are clear candidates for the understanding of …
On the limiters of two-equation turbulence models
CH Park, SO Park - International Journal of Computational Fluid …, 2005 - Taylor & Francis
When two-equation turbulence models are used, unrealistically large values of turbulence
variables can appear due to the infringement of a realizability condition or to numerical error …
variables can appear due to the infringement of a realizability condition or to numerical error …
Flow reconstructions and aerodynamic shape optimization of turbomachinery blades by POD-based hybrid models
This study presented a hybrid model method based on proper orthogonal decomposition
(POD) for flow field reconstructions and aerodynamic design optimization. The POD basis …
(POD) for flow field reconstructions and aerodynamic design optimization. The POD basis …