Composite wing optimization design based on distributed computing

The high accuracy commercial FEA (finite element analysis) software was integrated with GA (genetic algorithm) to solve the composite wing optimization design for aeroelastic request. An optimization algorithm for composite wings was proposed that integrates the distributed computing with GA to enhance the efficiency. Taking the aileron and control surface reversal problem of a high-aspect-ratio composite wing as an example, the result shows that the algorithm can solve the complicated structure optimization problem in engineering.