模块化变形翼的模块离散化与加固

Ryan Perera, P. Paudel, John K. Kamel, F. Xi, P. Walsh
{"title":"模块化变形翼的模块离散化与加固","authors":"Ryan Perera, P. Paudel, John K. Kamel, F. Xi, P. Walsh","doi":"10.5589/Q15-008","DOIUrl":null,"url":null,"abstract":"A morphing wing is designed to morph to different wing profiles required for different flight regimes. Such a design is based on modules, and discretization of different wing profiles will yield different sets of modules. In this paper, a novel wing module consolidation methodology is developed to consolidate different sets of modules to a common set of modules for a unified modular morphing wing design. Initial wing profiles are created for different flight regimes using an optimization algorithm coupled with a fluid solver. These wing profiles are then smoothened, and used as reference geometries for module discretization. The results of discretized wings are then consolidated using a sensitivity analysis and a weighting function that allows the designer to assign a higher priority to a specific flight regime. A case study, showing the implementation of this methodology for climb, cruise, and descent flight regimes, reveals that the consolidated wing can be morphed to approximate the original wing profi...","PeriodicalId":80861,"journal":{"name":"Canadian aeronautics and space journal. Le journal aeronautique et spatial du Canada","volume":"61 1","pages":"36-50"},"PeriodicalIF":0.0000,"publicationDate":"2015-10-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Module discretization and consolidation of a modular morphing wing\",\"authors\":\"Ryan Perera, P. Paudel, John K. Kamel, F. Xi, P. Walsh\",\"doi\":\"10.5589/Q15-008\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A morphing wing is designed to morph to different wing profiles required for different flight regimes. Such a design is based on modules, and discretization of different wing profiles will yield different sets of modules. In this paper, a novel wing module consolidation methodology is developed to consolidate different sets of modules to a common set of modules for a unified modular morphing wing design. Initial wing profiles are created for different flight regimes using an optimization algorithm coupled with a fluid solver. These wing profiles are then smoothened, and used as reference geometries for module discretization. The results of discretized wings are then consolidated using a sensitivity analysis and a weighting function that allows the designer to assign a higher priority to a specific flight regime. A case study, showing the implementation of this methodology for climb, cruise, and descent flight regimes, reveals that the consolidated wing can be morphed to approximate the original wing profi...\",\"PeriodicalId\":80861,\"journal\":{\"name\":\"Canadian aeronautics and space journal. Le journal aeronautique et spatial du Canada\",\"volume\":\"61 1\",\"pages\":\"36-50\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2015-10-07\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Canadian aeronautics and space journal. Le journal aeronautique et spatial du Canada\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.5589/Q15-008\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Canadian aeronautics and space journal. Le journal aeronautique et spatial du Canada","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5589/Q15-008","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

变形翼是设计为不同的飞行制度所需的不同的机翼轮廓。这种设计是基于模块的,不同翼型的离散化将产生不同的模块组。本文提出了一种新的机翼模块整合方法,将不同的模块整合为一组通用的模块,从而实现统一的模块化变形翼设计。使用优化算法和流体求解器为不同的飞行状态创建初始翼型。然后对这些机翼轮廓进行平滑处理,并用作模块离散化的参考几何形状。然后,使用灵敏度分析和加权函数将离散机翼的结果进行整合,从而允许设计师为特定的飞行状态分配更高的优先级。一个案例研究显示了这种方法在爬升、巡航和下降飞行状态下的实施,表明合并机翼可以变形到接近原始机翼的形状。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Module discretization and consolidation of a modular morphing wing
A morphing wing is designed to morph to different wing profiles required for different flight regimes. Such a design is based on modules, and discretization of different wing profiles will yield different sets of modules. In this paper, a novel wing module consolidation methodology is developed to consolidate different sets of modules to a common set of modules for a unified modular morphing wing design. Initial wing profiles are created for different flight regimes using an optimization algorithm coupled with a fluid solver. These wing profiles are then smoothened, and used as reference geometries for module discretization. The results of discretized wings are then consolidated using a sensitivity analysis and a weighting function that allows the designer to assign a higher priority to a specific flight regime. A case study, showing the implementation of this methodology for climb, cruise, and descent flight regimes, reveals that the consolidated wing can be morphed to approximate the original wing profi...
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
自引率
0.00%
发文量
0
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信