Real-Time Hybrid Testing of Strut-Braced Wing Under Aerodynamic Loading Using an Electrodynamic Actuator (2020)

First Author: Ruffini V

Attributed to: Digital twins for improved dynamic design funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1007/s40799-020-00394-5

Publication URI: http://dx.doi.org/10.1007/s40799-020-00394-5

Type: Journal Article/Review

Parent Publication: Experimental Techniques

Issue: 6