E Dick, S Kubacki - … Journal of Turbomachinery, Propulsion and Power, 2017 - mdpi.com
Current models for transition in turbomachinery boundary layer flows are reviewed. The basic physical mechanisms of transition processes and the way these processes are …
A methodology to implement non-reflecting boundary conditions for turbomachinery applications, based on characteristic analysis is described in this paper. For these …
RD Sandberg, V Michelassi - Flow, Turbulence and Combustion, 2019 - Springer
Over the past two decades high-fidelity simulations have become feasible for most main gas path turbomachinery components. This paper introduces the key challenges of simulating …
X Ge, S Arolla, P Durbin - Flow, turbulence and combustion, 2014 - Springer
An intermittency model that is formulated in local variables is proposed for representing bypass transition in Reynolds-Averaged Navier-Stokes (RANS) computations. No external …
T Gianoli, JF Boussuge, P Sagaut… - … Journal for Numerical …, 2023 - Wiley Online Library
This article reports a procedure to implement as well as to validate non‐reflecting boundary conditions applied for turbomachinery simulations, using Navier–Stokes characteristic …
Z Yang - Propulsion and Power Research, 2019 - Elsevier
Transition from laminar flow to turbulent flow is of great practical interest as it occurs in many engineering flows and often plays a critical role in aerodynamics and heat transfer …
JS Wang, J Wu, JJ Wang - Experiments in Fluids, 2023 - Springer
The wake/boundary–layer interactions over a cylinder/airfoil configuration are investigated using hydrogen bubble visualization and time-resolved particle image velocimetry. The …
D Xiao, G Papadakis - Physics of fluids, 2017 - pubs.aip.org
The central aim of the paper is to apply and assess a nonlinear optimal control strategy to suppress bypass transition, due to bimodal interactions [TA Zaki and PA Durbin,“Mode …
L Jia, T Zou, Y Zhu, C Lee - Physics of Fluids, 2018 - pubs.aip.org
This paper examines the transition process in a boundary layer on a rotor blade under the impingement of an inlet guide vane wake. The effects of wake strengths and the reduced …