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