Inerter-Based Configurations for Main-Landing-Gear Shimmy Suppression (2017)
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.c033964
Publication URI: http://dx.doi.org/10.2514/1.c033964
Type: Journal Article/Review
Parent Publication: Journal of Aircraft
Issue: 2