Advanced Thick FGM Plate–Cylindrical Shells in Supersonic Air Flow by Navier–Stokes Equation Analytical–Numerical Flow Model
The thermal vibrations of a thick-walled functionally graded material (FGM) plate–cylindrical shells in unsteady supersonic flow with a Navier–Stokes equation analytical–numerical flow model and third-order shear deformation theory (TSDT) displacement models are investigated. The aerodynamic pressur...
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| Format: | Artigo |
| Sprache: | Inglês |
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MDPI AG
2026-03-01
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| Schriftenreihe: | Computation |
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| Online-Zugang: | https://www.mdpi.com/2079-3197/14/3/66 |
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