30th Congress of the International Council of the Aeronautical Sciences

03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE

R. Zhang, Chinese Aeronautical Establishment, China; D.-G. Cui, Aviation of China, China; G. Song, Beihang University, China

This paper introduces a method to realize the fairing design of wing which could improve the performance of aerodynamic and manufacture. Through the definition of energy function of structure, the quick sensitivity analysis and genetic algorithm are combined to realize the optimization. The application of a composite wing proves the method’s efficiency.


View Paper