Wind Tunnel Investigations of a Pitch-Free Flexible High Aspect Ratio Aircraft Model (2024)
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/10.2514/6.2024-2819
Publication URI: http://dx.doi.org/10.2514/6.2024-2819
Type: Conference/Paper/Proceeding/Abstract