Research on stability of laminated composite plate under nonlinear aerodynamic load
In this paper, we propose an finite element approach based on classical plate theory to investigate the dynamic stability of a layered composite plate subject to nonlinear aerodynamic load. This study considers the influence of temperature, nonlinear geometry, and nonlinear aerodynamic load on compo...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2023-07-01
|
| Series: | Theoretical and Applied Mechanics Letters |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2095034923000326 |
| _version_ | 1827769015499489280 |
|---|---|
| author | The Van Tran Quoc Hoa Pham Nhan Thinh Hoang |
| author_facet | The Van Tran Quoc Hoa Pham Nhan Thinh Hoang |
| author_sort | The Van Tran |
| collection | DOAJ |
| description | In this paper, we propose an finite element approach based on classical plate theory to investigate the dynamic stability of a layered composite plate subject to nonlinear aerodynamic load. This study considers the influence of temperature, nonlinear geometry, and nonlinear aerodynamic load on composite plate structures simultaneously. Specifically, the present work conduct comparison the results of the critical pressure value between the nonlinear aerodynamic load and the linear aerodynamic load, thereby pointing out some necessary cases which must consider the nonlinearity of aerodynamic load for calculating the aerospace structures. We determine the critical pressure value and vibrational amplitude response of the plate by means of calculation. The outcomes of our calculations can be useful in designing and repairing body shells and wings of aircraft equipment. |
| first_indexed | 2024-03-11T12:19:25Z |
| format | Article |
| id | doaj.art-1b65c6b4465e45ecba61ea686a3aaff3 |
| institution | Directory Open Access Journal |
| issn | 2095-0349 |
| language | English |
| last_indexed | 2024-03-11T12:19:25Z |
| publishDate | 2023-07-01 |
| publisher | Elsevier |
| record_format | Article |
| series | Theoretical and Applied Mechanics Letters |
| spelling | doaj.art-1b65c6b4465e45ecba61ea686a3aaff32023-11-07T04:02:27ZengElsevierTheoretical and Applied Mechanics Letters2095-03492023-07-01134100461Research on stability of laminated composite plate under nonlinear aerodynamic loadThe Van Tran0Quoc Hoa Pham1Nhan Thinh Hoang2Faculty of Mechanical Engineering, Industrial University of Ho Chi Minh City, Ho Chi Minh City 700000, VietnamTran Dai Nghia University, Ho Chi Minh City, 700000, VietnamFaculty of Engineering and Technology, Nguyen Tat Thanh University, Ho Chi Minh City 700000, Vietnam; Corresponding authorIn this paper, we propose an finite element approach based on classical plate theory to investigate the dynamic stability of a layered composite plate subject to nonlinear aerodynamic load. This study considers the influence of temperature, nonlinear geometry, and nonlinear aerodynamic load on composite plate structures simultaneously. Specifically, the present work conduct comparison the results of the critical pressure value between the nonlinear aerodynamic load and the linear aerodynamic load, thereby pointing out some necessary cases which must consider the nonlinearity of aerodynamic load for calculating the aerospace structures. We determine the critical pressure value and vibrational amplitude response of the plate by means of calculation. The outcomes of our calculations can be useful in designing and repairing body shells and wings of aircraft equipment.http://www.sciencedirect.com/science/article/pii/S2095034923000326Finite element approachNonlinear aerodynamic loadComposite plate |
| spellingShingle | The Van Tran Quoc Hoa Pham Nhan Thinh Hoang Research on stability of laminated composite plate under nonlinear aerodynamic load Theoretical and Applied Mechanics Letters Finite element approach Nonlinear aerodynamic load Composite plate |
| title | Research on stability of laminated composite plate under nonlinear aerodynamic load |
| title_full | Research on stability of laminated composite plate under nonlinear aerodynamic load |
| title_fullStr | Research on stability of laminated composite plate under nonlinear aerodynamic load |
| title_full_unstemmed | Research on stability of laminated composite plate under nonlinear aerodynamic load |
| title_short | Research on stability of laminated composite plate under nonlinear aerodynamic load |
| title_sort | research on stability of laminated composite plate under nonlinear aerodynamic load |
| topic | Finite element approach Nonlinear aerodynamic load Composite plate |
| url | http://www.sciencedirect.com/science/article/pii/S2095034923000326 |
| work_keys_str_mv | AT thevantran researchonstabilityoflaminatedcompositeplateundernonlinearaerodynamicload AT quochoapham researchonstabilityoflaminatedcompositeplateundernonlinearaerodynamicload AT nhanthinhhoang researchonstabilityoflaminatedcompositeplateundernonlinearaerodynamicload |