Aeroelastic analysis and flutter control of wings and panels: A review
Abstract Flutter is a self‐excited vibration under the interaction of the inertial force, aerodynamic force, and elastic force of the structure. After the flutter occurs, the aircraft structures will exhibit limit cycle oscillation, which will cause catastrophic accidents or fatigue damage to the st...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-09-01
|
| Series: | International Journal of Mechanical System Dynamics |
| Subjects: | |
| Online Access: | https://doi.org/10.1002/msd2.12015 |
| _version_ | 1818288451036905472 |
|---|---|
| author | Yuyang Chai Wei Gao Benjamin Ankay Fengming Li Chuanzeng Zhang |
| author_facet | Yuyang Chai Wei Gao Benjamin Ankay Fengming Li Chuanzeng Zhang |
| author_sort | Yuyang Chai |
| collection | DOAJ |
| description | Abstract Flutter is a self‐excited vibration under the interaction of the inertial force, aerodynamic force, and elastic force of the structure. After the flutter occurs, the aircraft structures will exhibit limit cycle oscillation, which will cause catastrophic accidents or fatigue damage to the structures. Therefore, it is of great theoretical and practical significance to study the aeroelastic characteristics and flutter control for improving the aeroelastic stability of aircraft structures. This paper reviews the recent advances in aeroelastic analysis and flutter control of wings and panel structures. The mechanism of aeroelastic flutter of wings and panels is presented. The research methods of aeroelastic flutter for different structures developed in recent years are briefly summarized. Various control strategies including the linear and nonlinear control algorithms as well as the active flutter control results of wings and panels are presented. Finally, the paper ends with conclusions, which highlight challenges of the development in aeroelastic analysis and flutter control, and provide a brief outlook on the future investigations. This study aims to present a comprehensive understanding of aeroelastic analysis and flutter control. It can also provide guidance on the design of new wings and panel structures for improving their aeroelastic stability. |
| first_indexed | 2024-12-13T01:56:35Z |
| format | Article |
| id | doaj.art-8faa75975958404280968afc3bc19ca3 |
| institution | Directory Open Access Journal |
| issn | 2767-1402 |
| language | English |
| last_indexed | 2024-12-13T01:56:35Z |
| publishDate | 2021-09-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Mechanical System Dynamics |
| spelling | doaj.art-8faa75975958404280968afc3bc19ca32022-12-22T00:03:22ZengWileyInternational Journal of Mechanical System Dynamics2767-14022021-09-011153410.1002/msd2.12015Aeroelastic analysis and flutter control of wings and panels: A reviewYuyang Chai0Wei Gao1Benjamin Ankay2Fengming Li3Chuanzeng Zhang4Department of Engineering Mechanics, College of Aerospace and Civil Engineering Harbin Engineering University Harbin ChinaDepartment of Engineering Mechanics, College of Aerospace and Civil Engineering Harbin Engineering University Harbin ChinaDepartment of Civil Engineering University of Siegen Siegen GermanyDepartment of Engineering Mechanics, College of Aerospace and Civil Engineering Harbin Engineering University Harbin ChinaDepartment of Civil Engineering University of Siegen Siegen GermanyAbstract Flutter is a self‐excited vibration under the interaction of the inertial force, aerodynamic force, and elastic force of the structure. After the flutter occurs, the aircraft structures will exhibit limit cycle oscillation, which will cause catastrophic accidents or fatigue damage to the structures. Therefore, it is of great theoretical and practical significance to study the aeroelastic characteristics and flutter control for improving the aeroelastic stability of aircraft structures. This paper reviews the recent advances in aeroelastic analysis and flutter control of wings and panel structures. The mechanism of aeroelastic flutter of wings and panels is presented. The research methods of aeroelastic flutter for different structures developed in recent years are briefly summarized. Various control strategies including the linear and nonlinear control algorithms as well as the active flutter control results of wings and panels are presented. Finally, the paper ends with conclusions, which highlight challenges of the development in aeroelastic analysis and flutter control, and provide a brief outlook on the future investigations. This study aims to present a comprehensive understanding of aeroelastic analysis and flutter control. It can also provide guidance on the design of new wings and panel structures for improving their aeroelastic stability.https://doi.org/10.1002/msd2.12015aeroelastic analysisflutter controllimit cycle oscillationpanel structureswings |
| spellingShingle | Yuyang Chai Wei Gao Benjamin Ankay Fengming Li Chuanzeng Zhang Aeroelastic analysis and flutter control of wings and panels: A review International Journal of Mechanical System Dynamics aeroelastic analysis flutter control limit cycle oscillation panel structures wings |
| title | Aeroelastic analysis and flutter control of wings and panels: A review |
| title_full | Aeroelastic analysis and flutter control of wings and panels: A review |
| title_fullStr | Aeroelastic analysis and flutter control of wings and panels: A review |
| title_full_unstemmed | Aeroelastic analysis and flutter control of wings and panels: A review |
| title_short | Aeroelastic analysis and flutter control of wings and panels: A review |
| title_sort | aeroelastic analysis and flutter control of wings and panels a review |
| topic | aeroelastic analysis flutter control limit cycle oscillation panel structures wings |
| url | https://doi.org/10.1002/msd2.12015 |
| work_keys_str_mv | AT yuyangchai aeroelasticanalysisandfluttercontrolofwingsandpanelsareview AT weigao aeroelasticanalysisandfluttercontrolofwingsandpanelsareview AT benjaminankay aeroelasticanalysisandfluttercontrolofwingsandpanelsareview AT fengmingli aeroelasticanalysisandfluttercontrolofwingsandpanelsareview AT chuanzengzhang aeroelasticanalysisandfluttercontrolofwingsandpanelsareview |