基于涡环的改进提升线法及其在提升风机设计中的应用

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2022-01-01 DOI:10.2322/tjsass.65.23
Haitong Wang, Yan’gang Wang, Si Wang, Fang Zhou, Hanru Liu
{"title":"基于涡环的改进提升线法及其在提升风机设计中的应用","authors":"Haitong Wang, Yan’gang Wang, Si Wang, Fang Zhou, Hanru Liu","doi":"10.2322/tjsass.65.23","DOIUrl":null,"url":null,"abstract":"The image vortex model is widely used in lifting line method to predict the fl ow induced by the shroud and hub surface in ducted fan, but it does not perform well in lift fan design due to the zero far fi eld in fl ow. In this paper the theoretical defects and numerical error propagation characteristic of the image vortex model in simulating duct surface are studied. Then the vortex rings correction based on image vortex model is veri fi ed and applied in lifting line method. In order to test the improved method, a 150 mm diameter lift fan is designed by the modi fi ed lifting line method, after that, analyzed by the modi fi ed lifting line itself and RANS solver respectively. The results show that the contribution of the vortex rings at the rotor accounts for 50% of the total induced velocity, and it accounts for 35% at the stator, which veri fi es the necessity of the vortex rings correction. The performance of the rotor and stator geometry is consistent with the design expectation, the e ffi ciency is up to 90.97% by numerical simulation and 88.32% by experimental measurement, which con fi rms the reli-ability of the modi fi ed lifting line method developed in this paper especially on lift fan design.","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":0.7000,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design\",\"authors\":\"Haitong Wang, Yan’gang Wang, Si Wang, Fang Zhou, Hanru Liu\",\"doi\":\"10.2322/tjsass.65.23\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The image vortex model is widely used in lifting line method to predict the fl ow induced by the shroud and hub surface in ducted fan, but it does not perform well in lift fan design due to the zero far fi eld in fl ow. In this paper the theoretical defects and numerical error propagation characteristic of the image vortex model in simulating duct surface are studied. Then the vortex rings correction based on image vortex model is veri fi ed and applied in lifting line method. In order to test the improved method, a 150 mm diameter lift fan is designed by the modi fi ed lifting line method, after that, analyzed by the modi fi ed lifting line itself and RANS solver respectively. The results show that the contribution of the vortex rings at the rotor accounts for 50% of the total induced velocity, and it accounts for 35% at the stator, which veri fi es the necessity of the vortex rings correction. The performance of the rotor and stator geometry is consistent with the design expectation, the e ffi ciency is up to 90.97% by numerical simulation and 88.32% by experimental measurement, which con fi rms the reli-ability of the modi fi ed lifting line method developed in this paper especially on lift fan design.\",\"PeriodicalId\":54419,\"journal\":{\"name\":\"Transactions of the Japan Society for Aeronautical and Space Sciences\",\"volume\":\"1 1\",\"pages\":\"\"},\"PeriodicalIF\":0.7000,\"publicationDate\":\"2022-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Transactions of the Japan Society for Aeronautical and Space Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.2322/tjsass.65.23\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Transactions of the Japan Society for Aeronautical and Space Sciences","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2322/tjsass.65.23","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

摘要

升力线法中广泛采用像涡模型来预测导管式风机叶冠和轮毂表面诱导的气流,但由于气流中的远场为零,在升力风机设计中表现不佳。本文研究了像涡模型在模拟管道表面时的理论缺陷和数值误差传播特性。然后验证了基于图像涡模型的涡环校正方法,并将其应用于提升线法。为了验证改进后的方法,采用定矩提升线法设计了一个直径150mm的提升风机,然后分别用定矩提升线本身和RANS求解器进行了分析。结果表明,转子处涡流环的贡献占总感应速度的50%,定子处涡流环的贡献占总感应速度的35%,验证了涡流环校正的必要性。转子和定子几何形状的性能符合设计预期,数值模拟效率达90.97%,实验测量效率达88.32%,证实了本文提出的固定升力线方法特别是升力风机设计的可靠性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design
The image vortex model is widely used in lifting line method to predict the fl ow induced by the shroud and hub surface in ducted fan, but it does not perform well in lift fan design due to the zero far fi eld in fl ow. In this paper the theoretical defects and numerical error propagation characteristic of the image vortex model in simulating duct surface are studied. Then the vortex rings correction based on image vortex model is veri fi ed and applied in lifting line method. In order to test the improved method, a 150 mm diameter lift fan is designed by the modi fi ed lifting line method, after that, analyzed by the modi fi ed lifting line itself and RANS solver respectively. The results show that the contribution of the vortex rings at the rotor accounts for 50% of the total induced velocity, and it accounts for 35% at the stator, which veri fi es the necessity of the vortex rings correction. The performance of the rotor and stator geometry is consistent with the design expectation, the e ffi ciency is up to 90.97% by numerical simulation and 88.32% by experimental measurement, which con fi rms the reli-ability of the modi fi ed lifting line method developed in this paper especially on lift fan design.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
期刊最新文献
Acknowledgments to Associate Editors Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 71, No. 6, Dec. 2023) Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 6, Dec. 2022) Analysis of Rotorcraft Vibration Reduction Using a Center-of-Gravity Offset Investigation on Applying an InGaN Photocathode with Negative Electron Affinity for Electric Propulsion
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1