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