11   Artículos

 
en línea
Andrea Notaristefano, Giacomo Persico and Paolo Gaetani    
Turbulence intensity impacts the performance of turbine stages and it is an important inlet boundary condition for CFD computations; the knowledge of its value at the turbine inlet is then of paramount importance. In combustor?turbine interaction experim... ver más

 
en línea
Stephan Sundermeier, Maximilian Passmann, Stefan aus der Wiesche and Eugeny Y. Kenig    
In numerous turbomachinery applications, e.g., in aero-engines with regenerators for improving specific fuel consumption (SFC), heat exchangers with low-pressure loss are required. Pil low-plate heat exchangers (PPHE) are a novel exchanger type and promi... ver más

 
en línea
Lorenzo Casalino, Filippo Masseni and Dario Pastrone    
The optimal design of the propulsion system for a potential Mars Ascent Vehicle is analyzed, in the context of the Mars Sample Return Mission. The Mars Ascent Vehicle has to perform an initial ascent phase from the surface and then circularize into a 170... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Songsong Yu, Dayong Zhang and Qianjin Yue    
The jacket platform in the Bohai Sea oilfield is an important engineering development, offering design alternatives in this economically important region. However, ice-induced vibration in cold areas threatens the safety and operation of these platforms.... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Manuel Hildebrandt, Heiko Schwarz, Corina Schwitzke, Hans-Jörg Bauer and Jens Friedrichs    
Reducing losses in the secondary air system of gas and steam turbines can significantly increase the efficiency of such machines. Meanwhile, brush seals are a widely used alternative to labyrinth seals. Their most valuable advantage over other sealing co... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Fabrizio Fontaneto, Tony Arts, Matthieu Simon and Philippe Picot    
An extensive measurement campaign was carried out at the von Karman Institute for Fluid Dynamics to assess the aerodynamic performance of an ultra-low aspect ratio centripetal turbine stator. The test section consisted of 18 periodic sectors of two blade... ver más

 
usuarios registrados
Gervas Franceschini, Terry V. Jones and David R.H. Gillespie    
Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

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