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, Page 61-70 PDF (1.44 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2019.26466 | ||||
 View on SCiNiTO | ||||
| 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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