2   Artículos

 
en línea
Michael van de Noort and Peter Ireland    
The high pressure turbine nozzle guide vane of a modern aeroengine experiences large heat loads and thus requires both highly effective internal and external cooling. This can be accomplished with double-wall effusion cooling, which combines impingement,... ver más

 
en línea
Giovanna Barigozzi, Silvia Mosconi, Antonio Perdichizzi and Silvia Ravelli    
Hot streak migration in a linear vane cascade with showerhead film cooling was experimentally and numerically investigated at isentropic exit Mach number of Ma2is = 0.40, with an inlet turbulence intensity level of Tu1 = 9%. Two tangential positions of t... ver más

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