Discharge Coefficients of a Heavy Suspension Nozzle

The suspensions used in heavy vehicles often consist of several oil and two gas chambers. In order to perform an analytical study of the mass flow transferred between two gas chambers separated by a nozzle, and when considering the gas as compressible and real, it is usually needed to determine the...

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Main Authors: Carlos Rio-Cano, Navid M. Tousi, Josep M. Bergada, Angel Comas
Format: Article
Language:English
Published: MDPI AG 2021-03-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/11/6/2619
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author Carlos Rio-Cano
Navid M. Tousi
Josep M. Bergada
Angel Comas
author_facet Carlos Rio-Cano
Navid M. Tousi
Josep M. Bergada
Angel Comas
author_sort Carlos Rio-Cano
collection DOAJ
description The suspensions used in heavy vehicles often consist of several oil and two gas chambers. In order to perform an analytical study of the mass flow transferred between two gas chambers separated by a nozzle, and when considering the gas as compressible and real, it is usually needed to determine the discharge coefficient of the nozzle. The nozzle configuration analyzed in the present study consists of a T shape, and it is used to separate two nitrogen chambers employed in heavy vehicle suspensions. In the present study, under compressible dynamic real flow conditions and at operating pressures, discharge coefficients were determined based on experimental data. A test rig was constructed for this purpose, and air was used as working fluid. The study clarifies that discharge coefficients for the T shape nozzle studied not only depend on the pressure gradient between chambers but also on the flow direction. Computational Fluid Dynamic (CFD) simulations, using air as working fluid and when flowing in both nozzle directions, were undertaken, as well, and the fluid was considered as compressible and ideal. The CFD results deeply helped in understanding why the dynamic discharge coefficients were dependent on both the pressure ratio and flow direction, clarifying at which nozzle location, and for how long, chocked flow was to be expected. Experimentally-based results were compared with the CFD ones, validating both the experimental procedure and numerical methodologies presented. The information gathered in the present study is aimed to be used to mathematically characterize the dynamic performance of a real suspension.
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spelling doaj.art-397762603e2d447ab35f661c39511ebb2023-11-21T10:37:36ZengMDPI AGApplied Sciences2076-34172021-03-01116261910.3390/app11062619Discharge Coefficients of a Heavy Suspension NozzleCarlos Rio-Cano0Navid M. Tousi1Josep M. Bergada2Angel Comas3Mechanical Engineering Department, Universitat Politècnica de Catalunya, 08034 Barcelona, SpainFluid Mechanics Department, Universitat Politècnica de Catalunya, 08034 Barcelona, SpainFluid Mechanics Department, Universitat Politècnica de Catalunya, 08034 Barcelona, SpainHeat Engines Department, Universitat Politècnica de Catalunya, 08034 Barcelona, SpainThe suspensions used in heavy vehicles often consist of several oil and two gas chambers. In order to perform an analytical study of the mass flow transferred between two gas chambers separated by a nozzle, and when considering the gas as compressible and real, it is usually needed to determine the discharge coefficient of the nozzle. The nozzle configuration analyzed in the present study consists of a T shape, and it is used to separate two nitrogen chambers employed in heavy vehicle suspensions. In the present study, under compressible dynamic real flow conditions and at operating pressures, discharge coefficients were determined based on experimental data. A test rig was constructed for this purpose, and air was used as working fluid. The study clarifies that discharge coefficients for the T shape nozzle studied not only depend on the pressure gradient between chambers but also on the flow direction. Computational Fluid Dynamic (CFD) simulations, using air as working fluid and when flowing in both nozzle directions, were undertaken, as well, and the fluid was considered as compressible and ideal. The CFD results deeply helped in understanding why the dynamic discharge coefficients were dependent on both the pressure ratio and flow direction, clarifying at which nozzle location, and for how long, chocked flow was to be expected. Experimentally-based results were compared with the CFD ones, validating both the experimental procedure and numerical methodologies presented. The information gathered in the present study is aimed to be used to mathematically characterize the dynamic performance of a real suspension.https://www.mdpi.com/2076-3417/11/6/2619discharge coefficientsreal compressible flowComputational Fluid Dynamics (CFD)chocked flowanalytical solutions based on experimental data
spellingShingle Carlos Rio-Cano
Navid M. Tousi
Josep M. Bergada
Angel Comas
Discharge Coefficients of a Heavy Suspension Nozzle
Applied Sciences
discharge coefficients
real compressible flow
Computational Fluid Dynamics (CFD)
chocked flow
analytical solutions based on experimental data
title Discharge Coefficients of a Heavy Suspension Nozzle
title_full Discharge Coefficients of a Heavy Suspension Nozzle
title_fullStr Discharge Coefficients of a Heavy Suspension Nozzle
title_full_unstemmed Discharge Coefficients of a Heavy Suspension Nozzle
title_short Discharge Coefficients of a Heavy Suspension Nozzle
title_sort discharge coefficients of a heavy suspension nozzle
topic discharge coefficients
real compressible flow
Computational Fluid Dynamics (CFD)
chocked flow
analytical solutions based on experimental data
url https://www.mdpi.com/2076-3417/11/6/2619
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