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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