DECREASE OF DYNAMIC STRESSES LEVEL IN ROTOR BLADES OF THE TURBINE AT THE EXPENSE OF A OPTIMISATION OF NOZZLE VANES GEOMETRY
Interacting between the next rows of the turbine creates a circumferential flow non-uniformity, which leads to origination of resonance dynamic stresses on rotor bladings with frequencies z·fn, where fn - a rotor rotation frequency, z - number of stator vanes. At projection and development of the en...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
National Aerospace University «Kharkiv Aviation Institute»
2018-11-01
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| coleção: | Авіаційно-космічна техніка та технологія |
| Assuntos: | |
| Acesso em linha: | http://nti.khai.edu/ojs/index.php/aktt/article/view/529 |
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