Unstructured finite volume flow solver for the analysis of supersonic mixed - compression intakes /
حل الانسياب باستخدام الاحجام المحدودة متباينة الشكل لدراسة المداخل فوق الصوتية المختلطة
Ahmed Tawfeek Eltaweel ; Supervised Ali A.Hashem , Moumen M.Idres
- Cairo : Ahmed Tawfeek Eltaweel , 2007
- 111P : charts ; 30cm
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
Euler flow High resolution schemes Laminar flow Unstructured finite volume