000			02166cam a2200349 a 4500
003			EG-GiCUC
005			20250223032406.0
008			190925s2019 ua d f m 000 0 eng d
040			_aEG-GiCUC _beng _cEG-GiCUC
041	0		_aeng
049			_aDeposite
097			_aM.Sc
099			_aCai01.13.10.M.Sc.2019.Ho.H
100	0		_aHossam Hassan Alqaleiby Aboalela
245	1	0	_aHybrid level sets method/finite element flow solver for viscous flow simulations with moving boundaries / _cHossam Hassan Alqaleiby Aboalela ; Supervised Mohammed Samir Tosson , Ali Abdelfattah Hashem , Amr Gamal Guaily
246	1	5	_aنموذج مهجن بين طريقة مجموعة المستويات و طريقة العنصر المحدود لحل و محاكاة السريان اللزج في وجود حدود متحركة
260			_aCairo : _bHossam Hassan Alqaleiby Aboalela , _c2019
300			_a130 P. : _bcharts ; _c30cm
502			_aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mathematics and Physics
520			_aThe Fluid-Structural interaction between the flow field and the burning surface of a solid propellant rocket is investigated. The burning surface evolution geometry is captured using the level setsmethod. The flow field is modelled using different levels of complexity namely starting from a lumped mass (zero-dimensional unsteady) model till two-dimensional axisymmetric unsteady compressible viscous model.The coupling is applied successfully to the problem of internal ballistics of a solid rocket motor. The results are validated against available experimental work. Also, the coupling is applied successfully to the problem of wedge flow with a moving edge and shocks interactions
530			_aIssued also as CD
653		4	_aFinite element method
653		4	_aLevel set method
653		4	_aMoving boundary
700	0		_aAli Abdelfattah Hashem , _eSupervisor
700	0		_aAmr Gamal Guaily , _eSupervisor
700	0		_aMohammed Samir Tosson , _eSupervisor
856			_uhttp://172.23.153.220/th.pdf
905			_aNazla _eRevisor
905			_aShimaa _eCataloger
942			_2ddc _cTH
999			_c74126 _d74126