Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures
In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with orthotropic materials has been developed. A flat plate/shell finite element, which can model plate-like wings, has been accommodated to mode...
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| Published in | Aerospace science and technology Vol. 88; pp. 244 - 257 |
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| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Masson SAS
01.05.2019
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1270-9638 1626-3219 |
| DOI | 10.1016/j.ast.2019.03.025 |
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| Abstract | In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with orthotropic materials has been developed. A flat plate/shell finite element, which can model plate-like wings, has been accommodated to model composite/corrugated panels to investigate effects of different laminate orientations and corrugations. A corotational approach is used to consider the geometrical nonlinearity due to large deformation produced by wing morphing. An unsteady vortex-lattice method is implemented to couple with the structural model subject to the large deformations. A homogenization method is also implemented to model corrugated panels as equivalent orthotropic plates. Individual structural, aerodynamic, and corrugated panel models, as well as the complete nonlinear aeroelastic framework, are verified. Numerical studies explore the static aeroelastic responses of a flat wing with composite/corrugated panels. This work helps to understand the nonlinear aeroelastic characteristics of composite/corrugated wings and demonstrates the capability of the framework to analyze the nonlinear aeroelasticity of such morphing wings. |
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| AbstractList | In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with orthotropic materials has been developed. A flat plate/shell finite element, which can model plate-like wings, has been accommodated to model composite/corrugated panels to investigate effects of different laminate orientations and corrugations. A corotational approach is used to consider the geometrical nonlinearity due to large deformation produced by wing morphing. An unsteady vortex-lattice method is implemented to couple with the structural model subject to the large deformations. A homogenization method is also implemented to model corrugated panels as equivalent orthotropic plates. Individual structural, aerodynamic, and corrugated panel models, as well as the complete nonlinear aeroelastic framework, are verified. Numerical studies explore the static aeroelastic responses of a flat wing with composite/corrugated panels. This work helps to understand the nonlinear aeroelastic characteristics of composite/corrugated wings and demonstrates the capability of the framework to analyze the nonlinear aeroelasticity of such morphing wings. |
| Author | Su, Weihua Yokozeki, Tomohiro Tsushima, Natsuki Arizono, Hitoshi |
| Author_xml | – sequence: 1 givenname: Natsuki orcidid: 0000-0003-0767-7295 surname: Tsushima fullname: Tsushima, Natsuki email: tsushima.natsuki@jaxa.jp organization: Japan Aerospace Exploration Agency, Mitaka, Tokyo 181-0015, Japan – sequence: 2 givenname: Tomohiro surname: Yokozeki fullname: Yokozeki, Tomohiro organization: Department of Aeronautics and Astronautics, University of Tokyo, Hongo, Tokyo 113-8656, Japan – sequence: 3 givenname: Weihua orcidid: 0000-0002-4458-0524 surname: Su fullname: Su, Weihua organization: Department of Aerospace Engineering and Mechanics, University of Alabama, Box 870280, Tuscaloosa, AL 35487-0280, USA – sequence: 4 givenname: Hitoshi surname: Arizono fullname: Arizono, Hitoshi organization: Japan Aerospace Exploration Agency, Mitaka, Tokyo 181-0015, Japan |
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| Keywords | Finite elements Composites Corrugated panel Unsteady vortex-lattice method Morphing wing Nonlinear analysis |
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| Snippet | In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with... |
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| SubjectTerms | Composites Corrugated panel Finite elements Morphing wing Nonlinear analysis Unsteady vortex-lattice method |
| Title | Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures |
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