Computational aerodynamic analysis on perimeter reinforced (PR)-compliant wing
Implementing the morphing technique on a micro air vehicle (MAV) wing is a very challenging task, due to the MAV's wing size limitation and the complex morphing mechanism. As a result, understanding aerodynamic characteristics and flow configurations, subject to wing structure deformation of a...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Online Access: | View Fulltext in Publisher |