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3D INVISCID FLUTTER OF ROTOR BLADES AND STATOR/ROTOR STAGE
Numerical calculations of the 3D transonic flow of an ideal gas through turbomachinery rotor blade row and stator, rotor blades moving relatively one to another with taking into account the blades oscillations are presented. The approach is based on the solution of the coupled aerodynamic-structu...
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| Main Authors: | , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Gdańsk University of Technology
2001-10-01
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| Colecção: | TASK Quarterly |
| Assuntos: | |
| Acesso em linha: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/2281 |
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