Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method
In this paper, an analytical method is proposed to directly obtain the aeroelastic time domain response of the elastic boundary panel. Based on a modified Fourier series method (MFSM), the vibration analysis of elastic boundary panels is carried out, after the dynamics equation of the panel is obtai...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2019-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2019/5164026 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832545412811063296 |
|---|---|
| author | Xiyue Zhou Lifeng Wang Jingnong Jiang Zhu Su |
| author_facet | Xiyue Zhou Lifeng Wang Jingnong Jiang Zhu Su |
| author_sort | Xiyue Zhou |
| collection | DOAJ |
| description | In this paper, an analytical method is proposed to directly obtain the aeroelastic time domain response of the elastic boundary panel. Based on a modified Fourier series method (MFSM), the vibration analysis of elastic boundary panels is carried out, after the dynamics equation of the panel is obtained. Then, the vibrational functions are combined with the supersonic piston theory to establish the aeroelastic equation. The aeroelastic time domain response of the panel is obtained to analyze the flutter speed of the panel more intuitively. Finally, the flutter speeds of panels with different length-width ratios, thicknesses, and elastic boundary conditions are discussed in detail. |
| format | Article |
| id | doaj-art-f8a1795c9cb94551ae83d911446db076 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2019-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-f8a1795c9cb94551ae83d911446db0762025-02-03T07:26:05ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742019-01-01201910.1155/2019/51640265164026Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series MethodXiyue Zhou0Lifeng Wang1Jingnong Jiang2Zhu Su3State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaIn this paper, an analytical method is proposed to directly obtain the aeroelastic time domain response of the elastic boundary panel. Based on a modified Fourier series method (MFSM), the vibration analysis of elastic boundary panels is carried out, after the dynamics equation of the panel is obtained. Then, the vibrational functions are combined with the supersonic piston theory to establish the aeroelastic equation. The aeroelastic time domain response of the panel is obtained to analyze the flutter speed of the panel more intuitively. Finally, the flutter speeds of panels with different length-width ratios, thicknesses, and elastic boundary conditions are discussed in detail.http://dx.doi.org/10.1155/2019/5164026 |
| spellingShingle | Xiyue Zhou Lifeng Wang Jingnong Jiang Zhu Su Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method International Journal of Aerospace Engineering |
| title | Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method |
| title_full | Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method |
| title_fullStr | Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method |
| title_full_unstemmed | Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method |
| title_short | Hypersonic Aeroelastic Response of Elastic Boundary Panel Based on a Modified Fourier Series Method |
| title_sort | hypersonic aeroelastic response of elastic boundary panel based on a modified fourier series method |
| url | http://dx.doi.org/10.1155/2019/5164026 |
| work_keys_str_mv | AT xiyuezhou hypersonicaeroelasticresponseofelasticboundarypanelbasedonamodifiedfourierseriesmethod AT lifengwang hypersonicaeroelasticresponseofelasticboundarypanelbasedonamodifiedfourierseriesmethod AT jingnongjiang hypersonicaeroelasticresponseofelasticboundarypanelbasedonamodifiedfourierseriesmethod AT zhusu hypersonicaeroelasticresponseofelasticboundarypanelbasedonamodifiedfourierseriesmethod |