The use of micro-computers to investigate new solutions, tech-niques•and for training purposes, proved to be a cost effective solution. In this work the potential of using micro-computers to solve one dimensional transonic flow is explored. A newly developed implicit pseudo-unsteady finite difference method for solving Euler equations is considered. The equations are solved in a converging diverging nozzle. Solutions obtained are compared to the exact solution . Bounds on the different parameters affecting the solution process and time estimates for the algorithms considered are presented.
ABDELRAHMAN, M., & SHERIF, A. (2019). Calculation Of One-Dimensional Transonic Flows Using Micro-Computers. International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), 61-70. doi: 10.21608/asat.2019.26466
MLA
M. M. ABDELRAHMAN; A. O. SHERIF. "Calculation Of One-Dimensional Transonic Flows Using Micro-Computers", International Conference on Aerospace Sciences and Aviation Technology, 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, 2019, 61-70. doi: 10.21608/asat.2019.26466
HARVARD
ABDELRAHMAN, M., SHERIF, A. (2019). 'Calculation Of One-Dimensional Transonic Flows Using Micro-Computers', International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), pp. 61-70. doi: 10.21608/asat.2019.26466
VANCOUVER
ABDELRAHMAN, M., SHERIF, A. Calculation Of One-Dimensional Transonic Flows Using Micro-Computers. International Conference on Aerospace Sciences and Aviation Technology, 2019; 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO): 61-70. doi: 10.21608/asat.2019.26466
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