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Low-order Aeroelastic Modelling of a High Aspect Ratio Wing Aircraft Under Constrained Motion (2022)

First Author: Pontillo A

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