CFD simulation for the film cooling of gas turbine blades / Mohamed Samir Mohamed ; Supervised Essam E. Khalil , Hatem O. Haridy , Esmail M. Elbialy

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Mohamed Samir Mohamed

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Material type: Text

TextLanguage: English Publication details: Cairo : Mohamed Samir Mohamed , 2015Description: 67 P. : charts , facsimiles ; 30cmOther title:

دراسة عددية لنمذجة التبريد الغشائى من خلال الممرات لريش التوربينات الغازية [Added title page title]

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Issued also as CD

Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering- Department of Mechanical Power Engineering Summary: This research aims to study and analyze the heat transfer of fluid throughturbine blades. Internal cooling blades technique has been used to cool the gas turbine blades .Gas turbine blade cooling is used to save and protect the gas turbine from catastrophic failure due to high thermal stresses. 1, 550,000 of cells have been used to solve that problem. CFD has been used to evaluate the effect of cooling fluid flow rates into the blades on the flow coefficient. An optimization study using ANSYS has been studied to show the effect of the distance between holes and the best flow inlet angle for the cooling fluid through turbine blade

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Holdings
Item type	Current library	Home library	Call number	Copy number	Status	Date due	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.11.M.Sc.2015.Mo.C (Browse shelf(Opens below))		Not for loan		01010110067719000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.11.M.Sc.2015.Mo.C (Browse shelf(Opens below))	67719.CD	Not for loan		01020110067719000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering- Department of Mechanical Power Engineering

This research aims to study and analyze the heat transfer of fluid throughturbine blades. Internal cooling blades technique has been used to cool the gas turbine blades .Gas turbine blade cooling is used to save and protect the gas turbine from catastrophic failure due to high thermal stresses. 1, 550,000 of cells have been used to solve that problem. CFD has been used to evaluate the effect of cooling fluid flow rates into the blades on the flow coefficient. An optimization study using ANSYS has been studied to show the effect of the distance between holes and the best flow inlet angle for the cooling fluid through turbine blade

Issued also as CD

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