Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing

A composite high-aspect-ratio wing of a high-altitude long-endurance (HALE) aircraft was modeled with FEM by MSC/NASTRAN, and the nonlinear static equilibrium state is calculated under design load with follower force effect, but without load redistribution. Assuming the little vibration amplitude of...

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Bibliographic Details
Main Authors: Chang Chuan Xie, Jia Zhen Leng, Chao Yang
Format: Article
Language:English
Published: Wiley 2008-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2008/957561
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