Evaluation of Two-Hinged Wings

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/tjsass.64.267
Shun Watanabe, S. Sunada, K. Yamaguchi
{"title":"Evaluation of Two-Hinged Wings","authors":"Shun Watanabe, S. Sunada, K. Yamaguchi","doi":"10.2322/tjsass.64.267","DOIUrl":null,"url":null,"abstract":"Two types of wing geometries imitating wings of birds in gliding fl ight are analyzed with the vortex lattice method in terms of lift-drag ratio and root bending moment while varying the joint positions and joint angles under the constant lift coe ffi cient and constant fl ight velocity conditions. One geometry is, what is sometimes called, a gull wing which has a dihedral inner wing and horizontal outer wing, named “ DH wing. ” On the contrary, the other geometry is a drooped wing which has a horizontal inner wing and anhedral outer wing, named “ HA wing. ” The lift-drag ratio of the HA wing becomes larger when the joint of the anhedral outer wing is closer to the wing tip with a larger anhedral angle, while the root bending moment of the HA wing becomes smaller when the joint of the anhedral outer wing is closer to the wing root with a larger anhedral angle. In contrast, the DH wing has no combination of a joint position and joint angle to improve the lift-drag ratio, and it is found that the HA wing e ff ectively contributes to the reduction of the root bending moment and the lift-drag ratio compared with the DH wing.","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":0.7000,"publicationDate":"2021-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","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.64.267","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: 1

Abstract

Two types of wing geometries imitating wings of birds in gliding fl ight are analyzed with the vortex lattice method in terms of lift-drag ratio and root bending moment while varying the joint positions and joint angles under the constant lift coe ffi cient and constant fl ight velocity conditions. One geometry is, what is sometimes called, a gull wing which has a dihedral inner wing and horizontal outer wing, named “ DH wing. ” On the contrary, the other geometry is a drooped wing which has a horizontal inner wing and anhedral outer wing, named “ HA wing. ” The lift-drag ratio of the HA wing becomes larger when the joint of the anhedral outer wing is closer to the wing tip with a larger anhedral angle, while the root bending moment of the HA wing becomes smaller when the joint of the anhedral outer wing is closer to the wing root with a larger anhedral angle. In contrast, the DH wing has no combination of a joint position and joint angle to improve the lift-drag ratio, and it is found that the HA wing e ff ectively contributes to the reduction of the root bending moment and the lift-drag ratio compared with the DH wing.
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
双铰翼的评价
在恒定升力系数和恒定飞行速度条件下,采用涡点阵法分析了两种模拟鸟类滑翔飞行的机翼几何形状在改变关节位置和关节角度时的升阻比和根部弯矩。一种几何形状是,有时被称为海鸥翼,它具有二面体的内翼和水平的外翼,称为“DH翼”。相反,另一种几何形状是内翼为水平,外翼为四面体的下垂翼,称为“HA翼”。当四面体外翼结合部靠近翼尖且棱角较大时,HA翼的升阻比增大,而当四面体外翼结合部靠近翼根且棱角较大时,HA翼的根部弯矩减小。相比之下,DH翼没有结合关节位置和关节角度来提高升阻比,研究发现,与DH翼相比,HA翼有效地降低了根部弯矩和升阻比。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 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