Development of aeroelastic modeling and analysis for wing camber morphing technology
As one of the morphing methods, wing camber morphing technology has received great attention. Starting from the relevant projects of morphing wing at home and abroad, the aeroelastic modeling and analysis means of the camber morphing technology are focused on in this paper. Static aeroelasticity, fl...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2023-08-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022226?st=article_issue |
| _version_ | 1797682265700958208 |
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| author | NI Yingge ZHAO Hui QIAO Shengjun LYU Yi |
| author_facet | NI Yingge ZHAO Hui QIAO Shengjun LYU Yi |
| author_sort | NI Yingge |
| collection | DOAJ |
| description | As one of the morphing methods, wing camber morphing technology has received great attention. Starting from the relevant projects of morphing wing at home and abroad, the aeroelastic modeling and analysis means of the camber morphing technology are focused on in this paper. Static aeroelasticity, flutter, dynamic aeroelasticity response and alleviation, optimization and control are analyzed. Different research means are evaluated from the perspective of structural model, aerodynamic model, coupling method, optimization method and control strategy. The technical difficulties currently facing are analyzed. The problems that are necessary to be further resolved, including the influence of the nonlinear behavior of the flexible skin on the aeroelasticity of the variable camber wing, the influence of actuator system on the aeroelasticity and the lack of a comprehensive aeroelastic modeling method that can handle different nonlinearity are pointed out in order to provide guidance for the further improvement of the camber morphing technology. |
| first_indexed | 2024-03-11T23:57:15Z |
| format | Article |
| id | doaj.art-7fbdfec40d12407db164708ee2cbea4b |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-03-11T23:57:15Z |
| publishDate | 2023-08-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-7fbdfec40d12407db164708ee2cbea4b2023-09-18T07:34:35ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902023-08-0114411710.16615/j.cnki.1674-8190.2023.04.0120230401Development of aeroelastic modeling and analysis for wing camber morphing technologyNI Yingge0ZHAO Hui1QIAO Shengjun2LYU Yi3School of Aircraft Engineering, Xi'an Aeronautical University, Xi'an 710077, ChinaSchool of Aircraft Engineering, Xi'an Aeronautical University, Xi'an 710077, ChinaSchool of Aircraft Engineering, Xi'an Aeronautical University, Xi'an 710077, ChinaSchool of Aircraft Engineering, Xi'an Aeronautical University, Xi'an 710077, ChinaAs one of the morphing methods, wing camber morphing technology has received great attention. Starting from the relevant projects of morphing wing at home and abroad, the aeroelastic modeling and analysis means of the camber morphing technology are focused on in this paper. Static aeroelasticity, flutter, dynamic aeroelasticity response and alleviation, optimization and control are analyzed. Different research means are evaluated from the perspective of structural model, aerodynamic model, coupling method, optimization method and control strategy. The technical difficulties currently facing are analyzed. The problems that are necessary to be further resolved, including the influence of the nonlinear behavior of the flexible skin on the aeroelasticity of the variable camber wing, the influence of actuator system on the aeroelasticity and the lack of a comprehensive aeroelastic modeling method that can handle different nonlinearity are pointed out in order to provide guidance for the further improvement of the camber morphing technology.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022226?st=article_issuecamber morphing technologyaeroelasticityflutteroptimizationcontrol |
| spellingShingle | NI Yingge ZHAO Hui QIAO Shengjun LYU Yi Development of aeroelastic modeling and analysis for wing camber morphing technology Hangkong gongcheng jinzhan camber morphing technology aeroelasticity flutter optimization control |
| title | Development of aeroelastic modeling and analysis for wing camber morphing technology |
| title_full | Development of aeroelastic modeling and analysis for wing camber morphing technology |
| title_fullStr | Development of aeroelastic modeling and analysis for wing camber morphing technology |
| title_full_unstemmed | Development of aeroelastic modeling and analysis for wing camber morphing technology |
| title_short | Development of aeroelastic modeling and analysis for wing camber morphing technology |
| title_sort | development of aeroelastic modeling and analysis for wing camber morphing technology |
| topic | camber morphing technology aeroelasticity flutter optimization control |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022226?st=article_issue |
| work_keys_str_mv | AT niyingge developmentofaeroelasticmodelingandanalysisforwingcambermorphingtechnology AT zhaohui developmentofaeroelasticmodelingandanalysisforwingcambermorphingtechnology AT qiaoshengjun developmentofaeroelasticmodelingandanalysisforwingcambermorphingtechnology AT lyuyi developmentofaeroelasticmodelingandanalysisforwingcambermorphingtechnology |