Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme /
Mohammed Sayed Saleh Elsayed Kamel
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
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
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
Computional Fluid Dynamics Finite Volume Scramjet Engine
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
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
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
Computional Fluid Dynamics Finite Volume Scramjet Engine