Low-order Aeroelastic Modelling of a High Aspect Ratio Wing Aircraft Under Constrained Motion (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/10.2514/6.2022-1306
Publication URI: http://dx.doi.org/10.2514/6.2022-1306
Type: Conference/Paper/Proceeding/Abstract