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