Analysis of aspect and taper ratio on aeroelastic stability of composite shells

Analysis of aspect and taper ratio on aeroelastic stability of composite shells

In the present paper, the dynamic and static stability of composite shells for different aerodynamic configurations is investigated. Based on the existing models for flutter and torsional divergence, modified to include material anisotropy, stability parameters have been calculated for different asp...

Full description

Bibliographic Details
Main Authors: Dinulović Mirko, Rašuo Boško, Slavković Nikola, Karić Đorđe
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2022-01-01
Series:FME Transactions
Subjects:
static stability
divergence
flutter
dynamic stability
computational flutter analysis
composites
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2022/1451-20922204732D.pdf

Similar Items

Similar Items