23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada
Paper ICAS 2002-R11

BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED IN AIRCRAFT WING STRUCTURE ANALYSIS
D. Cui (1), Z. Li (1), Y. Xiu (1), J. He (2)
(1) Beijing University of Aeronautics & Astronautics, PRC; PRC Aviation Industry Corp., PRC; (2) China Aero Information Center, Beijing, PRC
Keywords: aero-elastic tailoring, design and analysis of laminates, aircraft design

It is an interesting task to use unsymmetry and unbalance laminated composite to development wing structure. This research work is mainly to solve the problems in wing development using this type structure. The research work is including: a) To solve the deflection in manufactory cure process. b) The analysis tools for development for engineering application c) The application analysis for a wing structure.

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23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada Paper ICAS 2002-R11

BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED IN AIRCRAFT WING STRUCTURE ANALYSIS

D. Cui (1), Z. Li (1), Y. Xiu (1), J. He (2) (1) Beijing University of Aeronautics & Astronautics, PRC; PRC Aviation Industry Corp., PRC; (2) China Aero Information Center, Beijing, PRC

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23rd Congress of International Council of the Aeronautical Sciences, 8-13 September, 2002, Toronto, Canada
Paper ICAS 2002-R11

D. Cui (1), Z. Li (1), Y. Xiu (1), J. He (2)
(1) Beijing University of Aeronautics & Astronautics, PRC; PRC Aviation Industry Corp., PRC; (2) China Aero Information Center, Beijing, PRC