Wang Xiaozhe, Wan Zhiqiang, Yang Chao

DOI Number: N/A

Conference number: IFASD-2015-002

A high-efficiency aeroelastic optimization method based on Kriging model and genetic algorithm is presented, and the method is verified by aeroelastic optimization of composite wing. The accuracy of aeroelastic optimization based on Kriging model is analyzed and the framework of aeroelastic optimization base on Kriging model and genetic algorithm is presented. The feasibility of the method is verified by an example, and the effects of design variable number and constraint number on optimization efficiency and result are analyzed in detail.

Read the full paper here

In Categories: 2. IFASD 2015, Aeroelastic Optimisation
Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.