Calculation Of One-Dimensional Transonic Flows Using Micro-Computers | ||
International Conference on Aerospace Sciences and Aviation Technology | ||
Article 6, Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985, Pages 61-70 PDF (1.44 M) | ||
Document Type: Original Article | ||
DOI: 10.21608/asat.2019.26466 | ||
Authors | ||
M. M. ABDELRAHMAN1; A. O. SHERIF2 | ||
1Assistant Professor,Dpt.of Aercnautics,Cairo University,Egypt. | ||
2Associate Professor,Dpt.of Aercnautics,Cairo University,Egypt. | ||
Abstract | ||
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. | ||
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