Large Deformation Prediction of Wing Model and Geometric Nonlinear Aeroelastic Analysis
Author:
Affiliation:
1. Beihang University,School of Aeronautic Science and Engineering,Beijing,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10424034/10424037/10424458.pdf?arnumber=10424458
Reference21 articles.
1. Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
2. Numerical Continuation of Limit Cycle Oscillations and Bifurcations in High-Aspect-Ratio Wings
3. Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings
4. Critical behaviour of slender wing configurations
5. Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM
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