Unstructured finite volume flow solver for the analysis of supersonic mixed - compression intakes / Ahmed Tawfeek Eltaweel ; Supervised Ali A.Hashem , Moumen M.Idres
Language: Eng Publication details: Cairo : Ahmed Tawfeek Eltaweel , 2007Description: 111P : charts ; 30cmOther title:- حل الانسياب باستخدام الاحجام المحدودة متباينة الشكل لدراسة المداخل فوق الصوتية المختلطة [Added title page title]
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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.2007.Ah.U (Browse shelf(Opens below)) | Not for loan | 01010110046805000 | |||
CD - Rom | مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2007.Ah.U (Browse shelf(Opens below)) | 46805.CD | Not for loan | 01020110046805000 |
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Cai01.13.01.M.Sc.2006.اح.ا اطار فكرى لمنظومة التنمية الصناعية فى مصر مع التطبيق على صناعة الطائرات / | Cai01.13.01.M.Sc.2007.Ah.M Modeling land cover induced climate changes using satellite data / | Cai01.13.01.M.Sc.2007.Ah.M Modeling land cover induced climate changes using satellite data / | Cai01.13.01.M.Sc.2007.Ah.U Unstructured finite volume flow solver for the analysis of supersonic mixed - compression intakes / | Cai01.13.01.M.Sc.2007.Ah.U Unstructured finite volume flow solver for the analysis of supersonic mixed - compression intakes / | Cai01.13.01.M.Sc.2007.Ha.S Spacecraft preliminary configuration and sizing / | Cai01.13.01.M.Sc.2007.Ha.S Spacecraft preliminary configuration and sizing / |
Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering
A two - dimensional flow solver using upwind scheme on unstructured grids has been developed The procedure uses a dual mesh system The conserved variables stored at the vertices of the mesh
Issued also as CD
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