Influence of Different Thermal Boundary on Numerical Analysis of Aerodynamic Heat of Supersonic Wing

The aerodynamic heating effect of the aircraft during supersonic flight has a great impact on the structural strength and thermal protection design. The aerodynamic thermal environment in the real state needs to consider the coupling of the external flow field and the structure and the influence of...

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Bibliographic Details
Main Authors: Zhao Xuan, Sun Zhi, Lü Runmin, Sun Jianhong
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2019-10-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019089?st=article_issue