Numerical Investigations of Subscale Flexible High Aspect Ratio Aircraft on a Dynamic Wind Tunnel Rig (2023)
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/10.2514/6.2023-1559
Publication URI: http://dx.doi.org/10.2514/6.2023-1559
Type: Conference/Paper/Proceeding/Abstract