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Aerothermoelastic Analysis of Conical Shell in Supersonic Flow

The aerothermoelastic behavior of a conical shell in supersonic flow is studied in the paper. According to Love’s first approximation shell theory, the kinetic energy and strain energy of the conical shell are expressed and the aerodynamic model is established by using the linear piston theory with...

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Principais autores: Min Wang, Leilei Zeng, Changying Zhao, Shupeng Sun, Yang Yang
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2023-04-01
Serier:Applied Sciences
Fag:
aerothermoelasticity
flutter
conical shell
general constraint
Online adgang:https://www.mdpi.com/2076-3417/13/8/4850
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