Aerodynamic Optimization Design of the Rotor Blade of a Tilt-rotor Aircraft

The aerodynamic design of tilt-rotor needs to synthetically consider the different requirements in helicopter mode and fixed-wing aircraft mode. The multi-objective genetic algorithm based on Kriging surrogate model is used to establish an optimization design methods for aerodynamic shape of tilt-ro...

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Bibliographic Details
Main Authors: Sun Kaijun, Zhang Lian, Fu Yiwei, Yu Yueyang
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2019-06-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018110?st=article_issue