Results 21 to 30 of about 57,630 (294)

Open-rotor noise prediction with a RANS-informed analytical method [PDF]

open access: yes18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012
Analytical models are informed by a steady-state RANS calculation with mixing plane in order to predict turbomachinery noise with a short computing time; the method is tested on the example of a contra-rotating open-rotor propulsion system at take-off condition; the results are compared to these of an unsteady RANS calculation with the pressure far ...
Guerin, S.   +3 more
openaire   +8 more sources

An efficient Two-Layer wall model for accurate numerical simulations of aeronautical applications [PDF]

open access: yes, 2019
Two-Layer wall models have been widely studied since they allow wall modeled Large Eddy Simulationsof general non-equilibrium flows. However, they are plagued by two persistent problems, the "log-layermismatch" and the resolved Reynolds stresses inflow ...
Calafell Sandiumenge, Joan   +2 more
core   +1 more source

Finite volume - space-time discontinuous Galerkin method for the numerical simulation of compressible turbulent flow in time dependent domains

open access: yesEPJ Web of Conferences, 2017
The article is concerned with the numerical simulation of the compressible turbulent flow in time dependent domains. The mathematical model of flow is represented by the system of non-stationary Reynolds- Averaged Navier-Stokes (RANS) equations.
Česenek Jan
doaj   +1 more source

Exploring Geometric Feature Hyper-Space in Data to Learn Representations of Abstract Concepts

open access: yesApplied Sciences, 2020
The term concept has been a prominent part of investigations in psychology and neurobiology where, mostly, it is mathematically or theoretically represented.
Rahul Sharma   +3 more
doaj   +1 more source

Grid resolution assessment method for hybrid RANS-LES in turbomachinery

open access: yesEngineering Applications of Computational Fluid Mechanics, 2022
Hybrid RANS-LES is a promising method for analyzing the complex flow structure in turbomachinery due to its excellent compromise between accuracy and computational cost.
Ruiyu Li   +4 more
doaj   +1 more source

Finite volume - space-time discontinuous Galerkin method for the solution of compressible turbulent flow

open access: yesEPJ Web of Conferences, 2016
In this article we deal with numerical simulation of the non-stationary compressible turbulent flow. Compressible turbulent flow is described by the Reynolds-Averaged Navier-Stokes (RANS) equations.
Česenek Jan
doaj   +1 more source

On Interface Issues in LES/RANS Coupling Strategies: A Method for Turbulence Forcing

open access: yesJournal of Fluid Science and Technology, 2011
The present work deals with a computational strategy coupling near-wall, eddyviscosity-based RANS models with LES within a zonal Hybrid LES/RANS (HLR) framework. Key questions concerning the coupling of both methods, the inherently steady RANS method and
Suad JAKIRLIC   +2 more
doaj   +1 more source

Construction method for general phenomenological RANS turbulence model

open access: yes, 2021
This paper proposes a phenomenological Reynolds Averaged Navier-Stokes (RANS) calculation model based on physical constraints. In this model part of the source terms in the e equation was replaced with the deep learning model, using the standard k-e model as a template.
Zhang, Shuming   +4 more
openaire   +2 more sources

Compressibility Modified RANS Simulations for Noise Prediction of Jet Exhausts with Chevron

open access: yesJournal of Applied Fluid Mechanics, 2021
The impact of compressibility modified RANS turbulence closures is investigated for high subsonic round and chevron jet flows with Mach = 0.9 and Re = 1.03×106, including the predicted acoustic noise generation.
Y. Jin, X. Han, P. Fan
doaj  

Modelling a Propeller Using Force and Mass Rate Density Fields

open access: yesJournal of Marine Science and Engineering, 2018
A method to replace a propeller by force and mass rate density fields has been developed. The force of the propeller on the flow is calculated using a boundary element method (BEM) program and used to generate the force and mass rate fields in a Reynolds-
David Hally
doaj   +1 more source

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