03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS
L.-J. Dong, Chinese Aeronautical Establishment, China; G. Song, Beijing University of Aeronautics and Astronautics, China; D.-G. Cui, Aircraft Design and Research Institute of Shenyang, China
This paper introduces a method of analyzing buckling/ post-buckling property of composite stiffened panels, combining with engineering method, and provides a strategy for stability safety margin analysis of panels under complex loading.