Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme / Mohammed Sayed Saleh Elsayed Kamel ; Supervised Ali A. Hashem , Farouk M. Owis , Moumen M. Idris
Material type: TextLanguage: eng Publication details: Cairo : Mohammed Sayed Saleh Elsayed Kamel , 2009Description: 159P. : charts , facsimiles ; 30cmOther title:- التحليل العددى للسريان المضطرب المتفاعل كيميائيا فى المحركات الصدمية فوق الصوتية باستخدام طريقة الاحجام المحدودة اللاضمنية النقطية [Added title page title]
- Issued also as CD
Item type | Current library | Home library | Call number | Copy number | Status | Date due | Barcode | |
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Thesis | قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2009.Mo.N (Browse shelf(Opens below)) | Not for loan | 01010110051157000 | |||
CD - Rom | مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2009.Mo.N (Browse shelf(Opens below)) | 51157.CD | Not for loan | 01020110051157000 |
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
Issued also as CD
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