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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2022-01-01
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Series: | FME Transactions |
Subjects: | |
Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2022/1451-20922204732D.pdf |