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 …
X Zheng, C Liu, F Liu, CI Yang - International Journal for …, 1998 - Wiley Online Library
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 …
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 …
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 …
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 …
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 …
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 …
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 …
JQ Luo, YL Zhu, X Tang, F Liu - Science China Technological Sciences, 2017 - Springer
This study presented a hybrid model method based on proper orthogonal decomposition (POD) for flow field reconstructions and aerodynamic design optimization. The POD basis …