THE INLET VORTEX VARIATION THROUGH A DECELERATED CASCADE AND ITS INFLUENCE ON THE PERFORMANCE OF AN AXIAL-FLOW TURBOMACHINE
- Author
- VELENSEK B
TURBOINSTITUT,LUBLJANA 61210,YUG - Source
- CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 2; PP. 1242-1252; BIBL. 12 REF.
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- TURBOMACHINE AXIALE ECOULEMENT CASCADE PROFIL ECOULEMENT MERIDIEN METHODE SINGULARITE THEORIE TOURBILLONNAIRE COUCHE LIMITE TURBOMACHINE ECOULEMENT AXIAL POMPE AXIALE METHODE CALCUL CARACTERISTIQUE FONCTIONNEMENT ROTOR TURBOMACHINE INDUSTRIE MECANIQUE
- Keyword (en)
- AXIAL TURBOMACHINE FLOW AEROFOIL CASCADE MERIDIAN FLOW SINGULARITY METHOD BOUNDARY LAYER TURBOMACHINE AXIAL FLOW AXIAL PUMP CALCULATING METHOD PERFORMANCE CHARACTERISTIC TURBOMACHINERY ROTOR MECHANICAL ENGINEERING
- Keyword (es)
- INDUSTRIA MECANICA
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design
- Discipline
- Mechanical engineering. Mechanical construction. Handling Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL8030215032
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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