ID 1570

 

Bend/Twist Coupling Effects for Unsymmetrical &

Unbalanced Laminates Used in Aircraft Wing Structure

 

 

Degang Cui, Zhengneng Li and Junyi He*

Aircraft Research Center, Beijing University of Aeronautics & Astronautics

*China Aero Information Center

Beijing China

 

Keywords: aero-elastic tailoring, laminated design, laminate analysis, aircraft design