Passive Gust Loads Alleviation in a Truss-Braced Wing Using an Inerter-Based Device (2019)

First Author: Szczyglowski C
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.c035452

Publication URI: http://dx.doi.org/10.2514/1.c035452

Type: Journal Article/Review

Parent Publication: Journal of Aircraft

Issue: 6

ISSN: 15333868 00218669