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Unstructured finite volume flow solver for the analysis of supersonic mixed - compression intakes / Ahmed Tawfeek Eltaweel ; Supervised Ali A.Hashem , Moumen M.Idres

By: Contributor(s): 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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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering Summary: 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
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis 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 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

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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