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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
Staff Zu Site
Abstract In Staff Site
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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