11   Artículos

 
en línea
Luís P. N. Mendes, Ana M. C. Ricardo, Alexandre J. M. Bernardino and Rui M. L. Ferreira    
We present novel velocimetry algorithms based on the hybridization of correlation-based Particle Image Velocimetry (PIV) and a combination of Lucas?Kanade and Liu?Shen optical flow (OpF) methods. An efficient Aparapi/OpenCL implementation of those method... ver más
Revista: Water    Formato: Electrónico

 
en línea
Joshua D. Blake, Adrian Sescu, David Thompson and Yuji Hattori    
Large-eddy simulation (LES)-based jet noise predictions do not resolve the entire broadband noise spectra, often under-predicting high frequencies that correspond to un-resolved small-scale turbulence. The coupled LES-synthetic turbulence (CLST) model is... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ettore Bertolini, Paul Pieringer and Wolfgang Sanz    
The aim of this work is to study the influence of different subgrid-scale (SGS) closure models and inflow turbulence conditions on the boundary layer transition on the suction side of a highly loaded transonic turbine cascade in the presence of high free... ver más

 
en línea
Jean Al-Am, Vincent Clair, Alexis Giauque, Jérôme Boudet and Fernando Gea-Aguilera    
In the present paper, large eddy simulations are performed to study two different mechanisms of Fan/OGV broadband noise: airfoil self-noise and turbulence interaction noise. Firstly, the current study focuses on the prediction of airfoil self-noise from ... ver más

 
en línea
Artur K. Lidtke, Maarten Klapwijk and Thomas Lloyd    
Inflow turbulence is relevant for many engineering applications relating to noise generation, including aircraft wings, landing gears, and non-cavitating marine propellers. While modelling of this phenomenon is well-established for higher Mach number aer... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Pooneh Aref, Mehdi Ghoreyshi, Adam Jirasek and Matthew J. Satchell    
The flow physics modeling and validation of the Royal Aircraft Establishment (RAE) subsonic intake Model 2129 (M2129) are presented. This intake has an 18 inches long S duct with a 5.4 inches offset, an external and an internal lip, forward and rear exte... ver más
Revista: Aerospace    Formato: Electrónico

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