Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig (2019)
Attributed to:
Dynamic Design Tools For Understanding and Exploiting Nonlinearity in Structures
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/1.c034995
Publication URI: http://dx.doi.org/10.2514/1.c034995
Type: Journal Article/Review
Parent Publication: Journal of Aircraft
Issue: 3
ISSN: 15333868 00218669