000			01946cam a2200325 a 4500
003			EG-GiCUC
008			160510s2015 ua d f m 000 0 eng d
040			_aEG-GiCUC _beng _cEG-GiCUC
041	0		_aeng
049			_aDeposite
097			_aPh.D
099			_aCai01.13.11.Ph.D.2015.Al.N
100	0		_aAlaa Ahmed Mohamed Osman
245	1	0	_aNumerical analysis of an external store separation from a fighter aircraft / _cAlaa Ahmed Mohamed Osman ; Supervised Essam E. Khalil , Osama E. AbdEllatif , Amgad M. Bayoumy
246	1	5	_aالتحليل العددي لاسقاط المعلقات الخارجية من طائرة مقاتلة
260			_aCairo : _bAlaa Ahmed Mohamed Osman , _c2015
300			_a149 P. : _bcharts ; _c30cm
502			_aThesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
520			_aIn this thesis, a numerical simulation of a store separating from an aircraft has been studied and validated. A dynamic unstructured tetrahedral mesh approach is used to numerically solving the discretized three dimensional, inviscid and compressible Euler equations. The method used for computations of separation of an external store assuming quasi-steady flow condition. Computations of quasi-steady flow have been directly coupled to a six degree-of-freedom (6DOF) rigid-body motion code to generate store trajectories. Then the trajectory of the store after it's safely separation from the F-16 aircraft till it reaching the Earth's surface are presented and discussedusing MATLAB/Simulink platform
530			_aIssued also as CD
653		4	_aCFD Modeling
653		4	_aQuasi-steady Flow
653		4	_aTransonic Store Separation
700	0		_aAmgad M. Bayoumy , _eSupervisor
700	0		_aEssam E. Khalil , _eSupervisor
700	0		_aOsama E. Abdellatif , _eSupervisor
905			_aAml _eCataloger
905			_aNazla _eRevisor
942			_2ddc _cTH
999			_c56363 _d56363