Integrated strain actuation in aircraft with highly flexible composite wings
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2003.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2005
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| Online Access: | http://hdl.handle.net/1721.1/8001 |
| _version_ | 1811076475093254144 |
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| author | Brown, Eric L. (Eric Lee) |
| author2 | Carlos E.S. Cesnik. |
| author_facet | Carlos E.S. Cesnik. Brown, Eric L. (Eric Lee) |
| author_sort | Brown, Eric L. (Eric Lee) |
| collection | MIT |
| description | Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2003. |
| first_indexed | 2024-09-23T10:22:45Z |
| format | Thesis |
| id | mit-1721.1/8001 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T10:22:45Z |
| publishDate | 2005 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/80012019-04-11T05:19:21Z Integrated strain actuation in aircraft with highly flexible composite wings Brown, Eric L. (Eric Lee) Carlos E.S. Cesnik. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Mechanical Engineering. Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2003. Includes bibliographical references (p. 167-171). The purpose of this thesis is to provide a framework for the study of wing warping as a means of achieving multiple aeroelastic goals. Shape change is achieved by integrating anisotropic piezoelectric composites (APC) within the passive composite wing skin. The goals include the ability of integrated strain actuation (ISA) to provide sufficient wing deformation for roll maneuver, gust load alleviation, flutter suppression, and redistribution of maneuver loads. A nonlinear analysis tool was constructed to study the behavior of aircraft with highly flexible active wings undergoing large deformation. It combines a new large displacement, strain-based finite element beam formulation with a finite-state unsteady aerodynamics model and a thin-wall active beam cross section model. The tool was created with the flexibility to model different aircraft configurations, including unconventional ones such as joined wing designs. The effects of sweep and dihedral, as well as large deformations are taken into account in the calculation of aerodynamic loads. The strain-based finite element formulation allows for a simplified control design because the flexible degrees of freedom are easily accessible by strain gages. To support the evaluation of ISA performance, and to study the impact of vehicle size on performance, three representative conventional vehicles using aileron control are modeled. The vehicles are based on fielded unmanned aerial vehicles (UAV), representing low, medium, and high altitude classes. The ISA wings are modeled by replacing some of the passive composite plies in with APC. The active and passive vehicles are compared based on the goals stated above. The impact of the piezoelectric composite material properties on weight and performance is discussed. (cont.) The required property values are determined for making ISA a viable method for primary roll control and wing stability. Numerical results show that roll control without ailerons is possible using present actuator technology. Integrated strain actuation is also shown to significantly alleviate gust loading and increase the flutter speed. Peak maneuver stresses are significantly reduced through active lift redistribution. by Eric L. Brown. Sc.D. 2005-08-24T22:42:07Z 2005-08-24T22:42:07Z 2003 2003 Thesis http://hdl.handle.net/1721.1/8001 53368805 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 205 p. 13537650 bytes 13537404 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
| spellingShingle | Mechanical Engineering. Brown, Eric L. (Eric Lee) Integrated strain actuation in aircraft with highly flexible composite wings |
| title | Integrated strain actuation in aircraft with highly flexible composite wings |
| title_full | Integrated strain actuation in aircraft with highly flexible composite wings |
| title_fullStr | Integrated strain actuation in aircraft with highly flexible composite wings |
| title_full_unstemmed | Integrated strain actuation in aircraft with highly flexible composite wings |
| title_short | Integrated strain actuation in aircraft with highly flexible composite wings |
| title_sort | integrated strain actuation in aircraft with highly flexible composite wings |
| topic | Mechanical Engineering. |
| url | http://hdl.handle.net/1721.1/8001 |
| work_keys_str_mv | AT brownericlericlee integratedstrainactuationinaircraftwithhighlyflexiblecompositewings |