Flutter Optimization of a Wing–Engine System with Passive and Active Control Approaches
Author:
Affiliation:
1. Adana Alparslan Turkes Science and Technology University, 01250 Adana, Turkey
2. Middle East Technical University, 06800 Ankara, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference41 articles.
1. A review on non-linear aeroelasticity of high aspect-ratio wings
2. Flutter improvement of a thin walled wing-engine system by applying curvilinear fiber path
3. Nonlinear time domain and stability analysis of beams under partially distributed follower force
4. Aeroelastic Tailoring of a Representative Wing Box Using Tow-Steered Composites
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