Mohammed Sayed Saleh Elsayed Kamel <br/><br/>
Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme /  
 التحليل العددى للسريان المضطرب المتفاعل كيميائيا فى المحركات الصدمية فوق الصوتية باستخدام طريقة الاحجام المحدودة اللاضمنية النقطية 
Mohammed Sayed Saleh Elsayed Kamel ; Supervised Ali A. Hashem , Farouk M. Owis , Moumen M. Idris 
 - Cairo :   Mohammed Sayed Saleh Elsayed Kamel ,   2009 
 - 159P. :   charts , facsimiles ;   30cm 
<br/><br/>Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering 
<br/><br/> This study investigates the steady state two-dimensional flow in scramjet combustors.The flow is modeled by RANS approach,where chemical kinetics model is applied to compute the finite rates of chemical reactions due to the small residence time of species inside engine.Turbulence is modeled based on Boussinesq's assumption,using the Baldwin-Lomax algebraic model,taking into account Degani and Schiff modifications 
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<br/><br/><label>Subjects--Index Terms: </label>Computional Fluid Dynamics  Finite Volume Scramjet Engine