TY  - BOOK
AU  - Mohammed Sayed Saleh Elsayed Kamel
AU  - Ali Abdelfatah Hashem , 
AU  - Farouk Mohamed Owis , 
AU  - Moumen Mohamed Idris , 
TI  - Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme / 
PY  - 2009///
CY  - Cairo : 
PB  - Mohammed Sayed Saleh Elsayed Kamel , 
KW  - Computional Fluid Dynamics
KW  - Finite Volume
KW  - Scramjet Engine
N1  - Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering; Issued also as CD
N2  - 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
ER  -