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