A Whole Aircraft Aeroelastic Model for Evaluation of Propulsion System Idealizations (2022)

First Author: Colbert S
Attributed to:  Novel Aircraft Concepts and Their Effect Upon Structural Definition funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2022-3956

Publication URI: http://dx.doi.org/10.2514/6.2022-3956

Type: Conference/Paper/Proceeding/Abstract