ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS
Azab, M., Abdelrahman, M., Mustafa, M. (2007). ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS. EKB Journal Management System, 12(ASAT Conference, 29-31 May 2007), 1-11. doi: 10.21608/asat.2007.23884
Mohammad Baher Azab; M. M. Abdelrahman; M. I. Mustafa. "ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS". EKB Journal Management System, 12, ASAT Conference, 29-31 May 2007, 2007, 1-11. doi: 10.21608/asat.2007.23884
Azab, M., Abdelrahman, M., Mustafa, M. (2007). 'ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS', EKB Journal Management System, 12(ASAT Conference, 29-31 May 2007), pp. 1-11. doi: 10.21608/asat.2007.23884
Azab, M., Abdelrahman, M., Mustafa, M. ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS. EKB Journal Management System, 2007; 12(ASAT Conference, 29-31 May 2007): 1-11. doi: 10.21608/asat.2007.23884

ON THE NUMERICAL SOLUTION OF THE INVISCID THREE DIMENSIONAL NON CIRCULAR NOZZLES WITH STRUCTURED NONORTHOGONAL GRIDS

International Conference on Aerospace Sciences and Aviation Technology
Article 18, Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Page 1-11  XML PDF (204.23 K)
Document Type: Original Article
DOI: 10.21608/asat.2007.23884
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Authors
Mohammad Baher Azab1; M. M. Abdelrahman2; M. I. Mustafa1
1Egyptian Armed Forces.
2Professor, Aerospace engineering department, Cairo University, Cairo, Egypt.
Abstract
A method is presented for solving three dimensional inviscid internal flows, with application to three dimensional noncircular nozzles. Spatial discretization is made on the finite difference formulation of Euler’s equations. The convective terms is differenced using the Van Leer flux vector splitting technique. Time is advanced using the implicit Euler backward time stepping. The resulting system of algebraic equations is solved using ADI method. New numerical treatment of the flow boundary conditions is presented and applied to handle the complicated mixed boundary conditions. Application to solve flow through nozzles shows good agreement with analytical results.
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