Optimal Design of Nozzle Based on Multi-fidelity Surrogate Model

The nozzle is one of the key components in the integrated design of the aircraft body/propulsion,which directly affects the thrust-drag matching and pitching moment matching and other characteristics of the aircraft.In order to improve the efficiency of the optimal design of the nozzle,a multi-objec...

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Bibliographic Details
Main Authors: LIU Jing, BIAN Xiao, XU Guanfeng, LI Shu, WANG Jianlin
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2022-12-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022002?st=article_issue

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