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Optimum Wing Shape Determination of Highly Flexible Morphing Aircraft for Improved Flight Performance
In this paper, optimum wing bending and torsion deformations are explored for a mission adaptive, highly flexible morphing aircraft. The complete highly flexible aircraft is modeled using a strain-based geometrically nonlinear beam formulation, coupled with unsteady aerodynamics and 6-dof rigid-body...
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| 發表在: | J Aircr |
|---|---|
| Main Authors: | , , |
| 格式: | Artigo |
| 語言: | Inglês |
| 出版: |
2016
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| 主題: | |
| 在線閱讀: | https://ncbi.nlm.nih.gov/pmc/articles/PMC5770154/ https://ncbi.nlm.nih.gov/pubmed/29348697 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.2514/1.C033490 |
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