Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment
In order to determine the significance and importance order of the jet performance caused by fan nozzle's geometric parameters of aero-engine online cleaning equipment, the orthogonal experiment method, standard k–ɛ turbulence model and volume of fluid (VOF) two-phase flow algorithm are used to...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2018-10-01
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Series: | The Journal of Engineering |
Subjects: | |
Online Access: | https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8971 |
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author | Xudong Shi Guijia Jiang Bing Wei Xiangfen Kong |
author_facet | Xudong Shi Guijia Jiang Bing Wei Xiangfen Kong |
author_sort | Xudong Shi |
collection | DOAJ |
description | In order to determine the significance and importance order of the jet performance caused by fan nozzle's geometric parameters of aero-engine online cleaning equipment, the orthogonal experiment method, standard k–ɛ turbulence model and volume of fluid (VOF) two-phase flow algorithm are used to research the jet of fan nozzle. The sensitivity of nozzle contraction angle, nozzle area ratio, nozzle incision angle, nozzle exit thickness and offset to the influence of fan nozzle spray angle was verified by range analysis and variance analysis. The results of the two analysis methods consistently show that the main order of influence of the geometric parameters of fan nozzle on spray angle is nozzle area ratio, nozzle incision angle, nozzle exit thickness, offset and nozzle convergence angle. The former two have more influence on the spray angle than the others. Finally, the simulation results and orthogonal test results are verified by the injection experiment of the fan nozzle. The jet shape is mainly determined by the nozzle area ratio and incision angle. The larger the incision angle and the nozzle area ratio are, the smaller the spray angle becomes. |
first_indexed | 2024-12-20T13:47:26Z |
format | Article |
id | doaj.art-ff542494e3da45698acdb9d54dde318d |
institution | Directory Open Access Journal |
issn | 2051-3305 |
language | English |
last_indexed | 2024-12-20T13:47:26Z |
publishDate | 2018-10-01 |
publisher | Wiley |
record_format | Article |
series | The Journal of Engineering |
spelling | doaj.art-ff542494e3da45698acdb9d54dde318d2022-12-21T19:38:37ZengWileyThe Journal of Engineering2051-33052018-10-0110.1049/joe.2018.8971JOE.2018.8971Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experimentXudong Shi0Guijia Jiang1Bing Wei2Xiangfen Kong3Civil Aviation University of ChinaCivil Aviation University of ChinaCivil Aviation University of ChinaCivil Aviation University of ChinaIn order to determine the significance and importance order of the jet performance caused by fan nozzle's geometric parameters of aero-engine online cleaning equipment, the orthogonal experiment method, standard k–ɛ turbulence model and volume of fluid (VOF) two-phase flow algorithm are used to research the jet of fan nozzle. The sensitivity of nozzle contraction angle, nozzle area ratio, nozzle incision angle, nozzle exit thickness and offset to the influence of fan nozzle spray angle was verified by range analysis and variance analysis. The results of the two analysis methods consistently show that the main order of influence of the geometric parameters of fan nozzle on spray angle is nozzle area ratio, nozzle incision angle, nozzle exit thickness, offset and nozzle convergence angle. The former two have more influence on the spray angle than the others. Finally, the simulation results and orthogonal test results are verified by the injection experiment of the fan nozzle. The jet shape is mainly determined by the nozzle area ratio and incision angle. The larger the incision angle and the nozzle area ratio are, the smaller the spray angle becomes.https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8971two-phase flowturbulenceflow simulationnozzlesaerospace enginesspraysjetsconfined flowvariance analysisfan nozzle jet performanceorthogonal experiment methodfan nozzle spray anglerange analysisgeometrical parameter effectfan nozzle contraction anglefan nozzle area ratiofan nozzle exit thicknessfan nozzle incision anglefan nozzle convergence angleaero-engine online cleaning equipmentstandard k–ε turbulence modelVOF two-phase flow algorithm |
spellingShingle | Xudong Shi Guijia Jiang Bing Wei Xiangfen Kong Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment The Journal of Engineering two-phase flow turbulence flow simulation nozzles aerospace engines sprays jets confined flow variance analysis fan nozzle jet performance orthogonal experiment method fan nozzle spray angle range analysis geometrical parameter effect fan nozzle contraction angle fan nozzle area ratio fan nozzle exit thickness fan nozzle incision angle fan nozzle convergence angle aero-engine online cleaning equipment standard k–ε turbulence model VOF two-phase flow algorithm |
title | Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
title_full | Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
title_fullStr | Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
title_full_unstemmed | Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
title_short | Research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
title_sort | research on geometrical parameters effect of fan nozzle jet performance based on orthogonal experiment |
topic | two-phase flow turbulence flow simulation nozzles aerospace engines sprays jets confined flow variance analysis fan nozzle jet performance orthogonal experiment method fan nozzle spray angle range analysis geometrical parameter effect fan nozzle contraction angle fan nozzle area ratio fan nozzle exit thickness fan nozzle incision angle fan nozzle convergence angle aero-engine online cleaning equipment standard k–ε turbulence model VOF two-phase flow algorithm |
url | https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8971 |
work_keys_str_mv | AT xudongshi researchongeometricalparameterseffectoffannozzlejetperformancebasedonorthogonalexperiment AT guijiajiang researchongeometricalparameterseffectoffannozzlejetperformancebasedonorthogonalexperiment AT bingwei researchongeometricalparameterseffectoffannozzlejetperformancebasedonorthogonalexperiment AT xiangfenkong researchongeometricalparameterseffectoffannozzlejetperformancebasedonorthogonalexperiment |