A New Mathematical Model for Coanda Effect Velocity Approximation

This paper addresses the problem of obtaining a set of mathematical equations that can accurately describe the velocity flow field near a cylindrical surface influenced by the Coandă effect. The work is relevant since the current state of the art Reynolds Averaged Navier Stokes models with curvature...

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Main Author: Valeriu DRĂGAN
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2012-12-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/dragan_v___v4_iss_4_full.pdf
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author Valeriu DRĂGAN
author_facet Valeriu DRĂGAN
author_sort Valeriu DRĂGAN
collection DOAJ
description This paper addresses the problem of obtaining a set of mathematical equations that can accurately describe the velocity flow field near a cylindrical surface influenced by the Coandă effect. The work is relevant since the current state of the art Reynolds Averaged Navier Stokes models with curvature correction do not completely describe the properties of the flow in accordance with the experimental data. Semi-empirical equations are therefore deduced based on experimental and theoretical state of the art. The resulting model is validated over a wider range of geometric layouts than any other existing semi-empirical model of its kind. The applications of this model are numerous, from super circulation wing calculations to fluidic devices such as actuators or fluidic diodes.
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spelling doaj.art-cdbf1b68255f4d8f9463b6e8385c1d772022-12-21T20:05:34ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282012-12-0144859210.13111/2066-8201.2012.4.4.7A New Mathematical Model for Coanda Effect Velocity ApproximationValeriu DRĂGANThis paper addresses the problem of obtaining a set of mathematical equations that can accurately describe the velocity flow field near a cylindrical surface influenced by the Coandă effect. The work is relevant since the current state of the art Reynolds Averaged Navier Stokes models with curvature correction do not completely describe the properties of the flow in accordance with the experimental data. Semi-empirical equations are therefore deduced based on experimental and theoretical state of the art. The resulting model is validated over a wider range of geometric layouts than any other existing semi-empirical model of its kind. The applications of this model are numerous, from super circulation wing calculations to fluidic devices such as actuators or fluidic diodes.http://bulletin.incas.ro/files/dragan_v___v4_iss_4_full.pdfCoanda effectfluidic deviceCEVAsuper circulationregressionsemi-empirical equationwall jet
spellingShingle Valeriu DRĂGAN
A New Mathematical Model for Coanda Effect Velocity Approximation
INCAS Bulletin
Coanda effect
fluidic device
CEVA
super circulation
regression
semi-empirical equation
wall jet
title A New Mathematical Model for Coanda Effect Velocity Approximation
title_full A New Mathematical Model for Coanda Effect Velocity Approximation
title_fullStr A New Mathematical Model for Coanda Effect Velocity Approximation
title_full_unstemmed A New Mathematical Model for Coanda Effect Velocity Approximation
title_short A New Mathematical Model for Coanda Effect Velocity Approximation
title_sort new mathematical model for coanda effect velocity approximation
topic Coanda effect
fluidic device
CEVA
super circulation
regression
semi-empirical equation
wall jet
url http://bulletin.incas.ro/files/dragan_v___v4_iss_4_full.pdf
work_keys_str_mv AT valeriudragan anewmathematicalmodelforcoandaeffectvelocityapproximation
AT valeriudragan newmathematicalmodelforcoandaeffectvelocityapproximation