Unsteady aerodynamics of a morphing tandem-wing unmanned aerial vehicle

The effects of unsteady aerodynamics for a tandem-wing unmanned aerial vehicle (UAV) prototype during the morphing stage have been investigated numerically at low Reynolds numbers (Re<10^6). The morphing stage consists of two stages. The first stage involves the unfolding of the canards and wings...

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Bibliographic Details
Main Authors: Zhang, G. Q., Yu, S. C. M.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2013
Online Access:https://hdl.handle.net/10356/85676
http://hdl.handle.net/10220/11677
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Institution: Nanyang Technological University
Language: English