Thermoelastic Response of Closed Cylindrical Shells in a Supersonic Gas Flow
The work is devoted to the investigation of flutter oscillations and the stability of the closed cylindrical shell in supersonic gas flow in an inhomogeneous temperature field. It is assumed that supersonic gas flows on the outside of the shell with an unperturbed velocity U, directed parallel to th...
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| Format: | Article |
| Language: | English |
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MDPI AG
2020-07-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/7/8/103 |