| 000 | 01957cam a2200313 a 4500 | ||
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| 003 | EG-GiCUC | ||
| 008 | 180213s2017 ua dh f m 000 0 eng d | ||
| 040 |
_aEG-GiCUC _beng _cEG-GiCUC |
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| 041 | 0 | _aeng | |
| 049 | _aDeposite | ||
| 097 | _aPh.D | ||
| 099 | _aCai01.13.11.Ph.D.2017.Mo.E | ||
| 100 | 0 | _aMohamed Ahmed Ibrahim Mohamed Khalifa | |
| 245 | 1 | 0 |
_aExperimental and numerical investigation of the effects of winglets on aircraft wings / _cMohamed Ahmed Ibrahim Mohamed Khalifa ; Supervised Abdelmotaleb Ali Mostafa , Osama Ezzat Abdellatif |
| 246 | 1 | 5 | _aدراسة عملية ونظرية عن تأثيرات الجنيحات على أجنحة الطـائرات |
| 260 |
_aCairo : _bMohamed Ahmed Ibrahim Mohamed Khalifa , _c2017 |
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| 300 |
_a141 P. : _bcharts , facsimiles ; _c30cm |
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| 502 | _aThesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering | ||
| 520 | _aExperimental and numerical investigation of the effects of winglets on an aircraft wing performance and structure is presented. A 3-D winglets analysis is performed on a civil aircraft wing. The study was divided into three stages. In the first stage, three wings using CFD software are numerically investigated. In the second stage, the aerodynamic characteristic around a civil aircraft wing are measured, and in the final stage, structure analysis using FEM is performed. The numerical results are in good agreement with experimental data and show blended connection enhances the lift coefficient appreciably. The structure results show composite material reduces wing weight | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aAircraft wing aerodynamic characteristics | |
| 653 | 4 | _aInduced drag | |
| 653 | 4 | _aWinglet | |
| 700 | 0 |
_aAbdelmotaleb Ali Mostafa , _eSupervisor |
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| 700 | 0 |
_aOsama Ezzat Abdellatif , _eSupervisor |
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| 905 |
_aNazla _eRevisor |
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| 905 |
_aShimaa _eCataloger |
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| 942 |
_2ddc _cTH |
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| 999 |
_c64976 _d64976 |
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