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Aeroelastic behaviour of the turbine blade row in 3D viscous flow
This paper presents the results of a numerical analysis of the aeroelastic behaviour of the oscillating blade row of a turbine stage in the 3D flow of viscous gas, taking into account the non-uniform pressure distribution in the circumferential direction behind the blade rotor. The numerical method...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English Russian Ukrainian |
| Published: |
Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
2018
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| Subjects: | |
| Online Access: | https://journals.uran.ua/jme/article/view/128156 |
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