Analysis of Flutter Characteristics for Composite Laminates in Hypersonic Yawed Flow

Analysis of Flutter Characteristics for Composite Laminates in Hypersonic Yawed Flow

This paper investigates the flutter characteristics of composite laminates in hypersonic yawed flow using numerical simulations. The governing equations are derived based on Hamilton’s principle and were discretized using the assumed mode method. The unsteady aerodynamic force is calculated by using...

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Bibliographic Details
Main Authors: Shuang Cao, Tongqing Guo, Jiangpeng Wu, Di Zhou, Ennan Shen
Format: Article
Language:English
Published: MDPI AG 2025-02-01
Series:Aerospace
Subjects:
thin-walled structures
composite laminates
flutter
yaw angle
critical dynamic pressure
limit cycle oscillation
Online Access:https://www.mdpi.com/2226-4310/12/3/174
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