Development, integration and testing of a 0-v honeycomb structure for aircraft morphing
This thesis lays out the development, analysis, integration and testing of a camber morphing concept for control surfaces dealing with fluidic dynamics, with specific focus on replacing the outboard aileron of fixed-wing aircraft in an effort to increase associated fuel efficiency. Core to the devel...
| Main Author: | |
|---|---|
| Published: |
University of Bristol
2015
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.690034 |