Computed Effect of Varying Tip Clearance and Axial Gap on Gas turbine Stage Performance Part (I): (Steady Flow)

Faculty Engineering Year: 2016
Type of Publication: ZU Hosted Pages:
Authors:
Mefreh Milad Nassif Ghabour
Journal: The Egyptian International Journal of Engineering Sciences and Technology The Egyptian International Journal of Engineering Sciences and Technology Volume:
Keywords : Computed Effect , Varying , Clearance , Axial , , , turbine    
Abstract:
It is desirable to further increase the efficiency of turbo-machines. In axial flow gas turbine, imprecise axial gap and tip clearance are two significant sources of inefficiency. This work investigates the effect of change in paramete
    
     
 
       

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