Loading…
二维水翼型空化流的数值计算
U6; In order to predict the effects of cavitation on a hydrofoil, the state equations of the cavitation model were combined with a linear viscous turbulent method for mixed fluids in the computational fluid dynamics (CFD) software FLUENT to simulate steady cavitating flow. At a fixed attack angle, p...
Saved in:
Published in: | 船舶与海洋工程学报(英文版) 2010, Vol.9 (1), p.63-68 |
---|---|
Main Authors: | , , , |
Format: | Article |
Language: | Chinese |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | |
---|---|
cites | |
container_end_page | 68 |
container_issue | 1 |
container_start_page | 63 |
container_title | 船舶与海洋工程学报(英文版) |
container_volume | 9 |
creator | 黄胜 何苗 王超 常欣 |
description | U6; In order to predict the effects of cavitation on a hydrofoil, the state equations of the cavitation model were combined with a linear viscous turbulent method for mixed fluids in the computational fluid dynamics (CFD) software FLUENT to simulate steady cavitating flow. At a fixed attack angle, pressure distributions and volume fractions of vapor at different cavitation numbers were simulated, and the results on foil sections agreed well with experimental data. In addition, at the various cavitation numbers, the vapor fractions at different attack angles were also predicted. The vapor region moved towards the front of the airfoil and the length of the cavity grew with increased attack angle. The results show that this method of applying FLUENT to simulate cavitation is reliable. |
doi_str_mv | 10.1007/s11804-010-8090-4 |
format | article |
fullrecord | <record><control><sourceid>wanfang_jour</sourceid><recordid>TN_cdi_wanfang_journals_hebgcdxxb_e201001010</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><wanfj_id>hebgcdxxb_e201001010</wanfj_id><sourcerecordid>hebgcdxxb_e201001010</sourcerecordid><originalsourceid>FETCH-wanfang_journals_hebgcdxxb_e2010010103</originalsourceid><addsrcrecordid>eNpjYJA0NNAzNDAw1y82NLQwMNE1MDTQtTCwNNA1YWHgNDQzN9S1NDE25mDgLS7OTDIwMjI2NLU0MuNkUH-yq-f57i3PNmx5vn_P03ndz1fuetoz7dnWxuezWp5N3fC0Yc-LdQufr5vOw8CalphTnMoLpbkZdNxcQ5w9dMsT89IS89Ljs_JLi_KAMvEZqUnpySkVFUnxqUZAVwCRoYExicoBT4dJ0A</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>二维水翼型空化流的数值计算</title><source>Springer Nature</source><creator>黄胜 ; 何苗 ; 王超 ; 常欣</creator><creatorcontrib>黄胜 ; 何苗 ; 王超 ; 常欣</creatorcontrib><description>U6; In order to predict the effects of cavitation on a hydrofoil, the state equations of the cavitation model were combined with a linear viscous turbulent method for mixed fluids in the computational fluid dynamics (CFD) software FLUENT to simulate steady cavitating flow. At a fixed attack angle, pressure distributions and volume fractions of vapor at different cavitation numbers were simulated, and the results on foil sections agreed well with experimental data. In addition, at the various cavitation numbers, the vapor fractions at different attack angles were also predicted. The vapor region moved towards the front of the airfoil and the length of the cavity grew with increased attack angle. The results show that this method of applying FLUENT to simulate cavitation is reliable.</description><identifier>ISSN: 1671-9433</identifier><identifier>DOI: 10.1007/s11804-010-8090-4</identifier><language>chi</language><ispartof>船舶与海洋工程学报(英文版), 2010, Vol.9 (1), p.63-68</ispartof><rights>Copyright © Wanfang Data Co. Ltd. All Rights Reserved.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://www.wanfangdata.com.cn/images/PeriodicalImages/hebgcdxxb-e/hebgcdxxb-e.jpg</thumbnail><link.rule.ids>314,776,780,4009,27902,27903,27904</link.rule.ids></links><search><creatorcontrib>黄胜</creatorcontrib><creatorcontrib>何苗</creatorcontrib><creatorcontrib>王超</creatorcontrib><creatorcontrib>常欣</creatorcontrib><title>二维水翼型空化流的数值计算</title><title>船舶与海洋工程学报(英文版)</title><description>U6; In order to predict the effects of cavitation on a hydrofoil, the state equations of the cavitation model were combined with a linear viscous turbulent method for mixed fluids in the computational fluid dynamics (CFD) software FLUENT to simulate steady cavitating flow. At a fixed attack angle, pressure distributions and volume fractions of vapor at different cavitation numbers were simulated, and the results on foil sections agreed well with experimental data. In addition, at the various cavitation numbers, the vapor fractions at different attack angles were also predicted. The vapor region moved towards the front of the airfoil and the length of the cavity grew with increased attack angle. The results show that this method of applying FLUENT to simulate cavitation is reliable.</description><issn>1671-9433</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNpjYJA0NNAzNDAw1y82NLQwMNE1MDTQtTCwNNA1YWHgNDQzN9S1NDE25mDgLS7OTDIwMjI2NLU0MuNkUH-yq-f57i3PNmx5vn_P03ndz1fuetoz7dnWxuezWp5N3fC0Yc-LdQufr5vOw8CalphTnMoLpbkZdNxcQ5w9dMsT89IS89Ljs_JLi_KAMvEZqUnpySkVFUnxqUZAVwCRoYExicoBT4dJ0A</recordid><startdate>2010</startdate><enddate>2010</enddate><creator>黄胜</creator><creator>何苗</creator><creator>王超</creator><creator>常欣</creator><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>2010</creationdate><title>二维水翼型空化流的数值计算</title><author>黄胜 ; 何苗 ; 王超 ; 常欣</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-wanfang_journals_hebgcdxxb_e2010010103</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>chi</language><creationdate>2010</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>黄胜</creatorcontrib><creatorcontrib>何苗</creatorcontrib><creatorcontrib>王超</creatorcontrib><creatorcontrib>常欣</creatorcontrib><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>船舶与海洋工程学报(英文版)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>黄胜</au><au>何苗</au><au>王超</au><au>常欣</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>二维水翼型空化流的数值计算</atitle><jtitle>船舶与海洋工程学报(英文版)</jtitle><date>2010</date><risdate>2010</risdate><volume>9</volume><issue>1</issue><spage>63</spage><epage>68</epage><pages>63-68</pages><issn>1671-9433</issn><abstract>U6; In order to predict the effects of cavitation on a hydrofoil, the state equations of the cavitation model were combined with a linear viscous turbulent method for mixed fluids in the computational fluid dynamics (CFD) software FLUENT to simulate steady cavitating flow. At a fixed attack angle, pressure distributions and volume fractions of vapor at different cavitation numbers were simulated, and the results on foil sections agreed well with experimental data. In addition, at the various cavitation numbers, the vapor fractions at different attack angles were also predicted. The vapor region moved towards the front of the airfoil and the length of the cavity grew with increased attack angle. The results show that this method of applying FLUENT to simulate cavitation is reliable.</abstract><doi>10.1007/s11804-010-8090-4</doi></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1671-9433 |
ispartof | 船舶与海洋工程学报(英文版), 2010, Vol.9 (1), p.63-68 |
issn | 1671-9433 |
language | chi |
recordid | cdi_wanfang_journals_hebgcdxxb_e201001010 |
source | Springer Nature |
title | 二维水翼型空化流的数值计算 |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T15%3A06%3A42IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-wanfang_jour&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=%E4%BA%8C%E7%BB%B4%E6%B0%B4%E7%BF%BC%E5%9E%8B%E7%A9%BA%E5%8C%96%E6%B5%81%E7%9A%84%E6%95%B0%E5%80%BC%E8%AE%A1%E7%AE%97&rft.jtitle=%E8%88%B9%E8%88%B6%E4%B8%8E%E6%B5%B7%E6%B4%8B%E5%B7%A5%E7%A8%8B%E5%AD%A6%E6%8A%A5%EF%BC%88%E8%8B%B1%E6%96%87%E7%89%88%EF%BC%89&rft.au=%E9%BB%84%E8%83%9C&rft.date=2010&rft.volume=9&rft.issue=1&rft.spage=63&rft.epage=68&rft.pages=63-68&rft.issn=1671-9433&rft_id=info:doi/10.1007/s11804-010-8090-4&rft_dat=%3Cwanfang_jour%3Ehebgcdxxb_e201001010%3C/wanfang_jour%3E%3Cgrp_id%3Ecdi_FETCH-wanfang_journals_hebgcdxxb_e2010010103%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rft_wanfj_id=hebgcdxxb_e201001010&rfr_iscdi=true |