Numerical computations of gas turbine combustion products effects on film cooling effectiveness /
Ibrahim Mohamed Hasan Sayed
Numerical computations of gas turbine combustion products effects on film cooling effectiveness / التحليل العددى لتأثير نواتج أحتراق توربينة غازية على كفاءه التبريد الغشائى Ibrahim Mohamed Hasan Sayed ; Supervised Essam Eldin Khalil , Gamal Abdelmenam Elhariry - Cairo : Ibrahim Mohamed Hasan Sayed , 2014 - 122 P. : facsimiles ; 30cm
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
Cooling technologies for gas turbine applications play an increasingly more important role. This is due to the high firing temperatures to meet the demand for higher performance turbine power. Film cooling is a technique employed to protect the external surface of gas turbine blades from the hot mainstream gas by ejecting the internal coolant air through discrete holes or slots at several locations on the blade exterior surface. Passing the coolant through conventional cylindrical holes causes protection for gas turbine blades from high temperatures. Early studies have proved that the results obtained on simple flat surfaces models can be applied to real engine design with slight corrections
Effectiveness Film cooling Turbine
Numerical computations of gas turbine combustion products effects on film cooling effectiveness / التحليل العددى لتأثير نواتج أحتراق توربينة غازية على كفاءه التبريد الغشائى Ibrahim Mohamed Hasan Sayed ; Supervised Essam Eldin Khalil , Gamal Abdelmenam Elhariry - Cairo : Ibrahim Mohamed Hasan Sayed , 2014 - 122 P. : facsimiles ; 30cm
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
Cooling technologies for gas turbine applications play an increasingly more important role. This is due to the high firing temperatures to meet the demand for higher performance turbine power. Film cooling is a technique employed to protect the external surface of gas turbine blades from the hot mainstream gas by ejecting the internal coolant air through discrete holes or slots at several locations on the blade exterior surface. Passing the coolant through conventional cylindrical holes causes protection for gas turbine blades from high temperatures. Early studies have proved that the results obtained on simple flat surfaces models can be applied to real engine design with slight corrections
Effectiveness Film cooling Turbine