Design and Assessment of Subscale Flexible High Aspect Ratio Cantilever Wings (2022)

First Author: Banneheka Navaratna P
Attributed to:  Experimental Flight Dynamics Testing for Highly Flexible Aircraft funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2022-1305

Publication URI: http://dx.doi.org/10.2514/6.2022-1305

Type: Conference/Paper/Proceeding/Abstract