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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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Vydáno v:J Aircr
Hlavní autoři: Su, Weihua, Swei, Sean Shan-Min, Zhu, Guoming G.
Médium: Artigo
Jazyk:Inglês
Vydáno: 2016
Témata:
On-line přístup: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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