8   Artículos

 
en línea
Valerie Hernley, Aleksandar Jemcov, Jeongseek Kang, Matthew Montgomery and Scott C. Morris    
The relationship between aerodynamic forcing and non-synchronous vibration (NSV) in axial compressors remains difficult to ascertain from experimental measurements. In this work, the relationship between casing pressure and blade vibration was investigat... ver más

 
en línea
Gyuzel Yakhina, Michel Roger, Stéphane Moreau, Lap Nguyen and Vladimir Golubev    
An experimental and analytical study of the tonal trailing-edge noise of a symmetric NACA-0012 aerofoil and of a cambered SD7003 aerofoil has been achieved. It provides a complete experimental database for both aerofoils and improves the understanding of... ver más
Revista: Acoustics    Formato: Electrónico

 
en línea
Constantin Tanasa, Alin Bosioc, Sebastian Muntean and Romeo Susan-Resiga    
In this paper, we introduce a novel passive control method to mitigate the unsteadiness effects associated to the swirling flows with self-induced instabilities. The control method involves a progressive throttling cross-section flow at the outlet of the... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Dario Valentini, Giovanni Pace, Angelo Pasini, Ruzbeh Hadavandi and Luca D?Agostino    
The paper presents an experimental campaign aimed at the characterization of the relationship between cavitation-induced instabilities and forces acting on the shaft, relevant to space application turbopumps. The experiments have been carried out on a si... ver más

 
en línea
Mario Eck, Silvio Geist and Dieter Peitsch    
Axial compressors in aero engines are prone to suffering a breakdown of orderly flow when operating at the peak of the pressure rise characteristic. The damaging potential of separated flows is why a safe distance has to be left between every possible op... ver más
Revista: Applied Sciences    Formato: Electrónico

 
usuarios registrados
R. Mailach, I. Lehmann, and K. Vogeler     Pág. 453 - 460
Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

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