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...
Main Authors: | , , , |
---|---|
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 |
_version_ | 1797541236096106496 |
---|---|
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. |
first_indexed | 2024-03-10T13:12:24Z |
format | Article |
id | doaj.art-397762603e2d447ab35f661c39511ebb |
institution | Directory Open Access Journal |
issn | 2076-3417 |
language | English |
last_indexed | 2024-03-10T13:12:24Z |
publishDate | 2021-03-01 |
publisher | MDPI AG |
record_format | Article |
series | Applied Sciences |
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 |
work_keys_str_mv | AT carlosriocano dischargecoefficientsofaheavysuspensionnozzle AT navidmtousi dischargecoefficientsofaheavysuspensionnozzle AT josepmbergada dischargecoefficientsofaheavysuspensionnozzle AT angelcomas dischargecoefficientsofaheavysuspensionnozzle |