Quasi-Steady Aeroelastic Analysis of the Semi-Aeroelastic Hinge Including Geometric Nonlinearities
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036115
Reference30 articles.
1. A Review of Morphing Aircraft
2. Optimization of a Scaled Sensorcraft Model with Passive Gust Alleviation
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4. Gust Alleviation of a Large Aircraft with a Passive Twist Wingtip
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