| 000 | 02014cam a2200337 a 4500 | ||
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| 003 | EG-GiCUC | ||
| 005 | 20250223031051.0 | ||
| 008 | 141011s2014 ua h f m 000 0 eng d | ||
| 040 |
_aEG-GiCUC _beng _cEG-GiCUC |
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| 041 | 0 | _aeng | |
| 049 | _aDeposite | ||
| 097 | _aM.Sc | ||
| 099 | _aCai01.13.11.M.Sc.2014.Ib.N | ||
| 100 | 0 | _aIbrahim Mohamed Hasan Sayed | |
| 245 | 1 | 0 |
_aNumerical computations of gas turbine combustion products effects on film cooling effectiveness / _cIbrahim Mohamed Hasan Sayed ; Supervised Essam Eldin Khalil , Gamal Abdelmenam Elhariry |
| 246 | 1 | 5 | _aالتحليل العددى لتأثير نواتج أحتراق توربينة غازية على كفاءه التبريد الغشائى |
| 260 |
_aCairo : _bIbrahim Mohamed Hasan Sayed , _c2014 |
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| 300 |
_a122 P. : _bfacsimiles ; _c30cm |
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| 502 | _aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering | ||
| 520 | _aCooling 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 | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aEffectiveness | |
| 653 | 4 | _aFilm cooling | |
| 653 | 4 | _aTurbine | |
| 700 | 0 |
_aEssam Eldin Khalil , _eSupervisor |
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| 700 | 0 |
_aGamal Abdelmenam Elhariry , _eSupervisor |
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| 856 | _uhttp://172.23.153.220/th.pdf | ||
| 905 |
_aNazla _eRevisor |
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| 905 |
_aSamia _eCataloger |
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| 942 |
_2ddc _cTH |
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| 999 |
_c47712 _d47712 |
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