| 摘要: |
| 本文介绍了亚燃、超燃双重燃烧进气分流的物理数学模型以及应用Euler方程组求解分流流场的数值计算方法,最后给出了计算的初步结果. |
| 关键词: 亚音速燃烧 超音速燃烧 空气流 分配 数值解 |
| DOI： |
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| NUMERICAL SIMULATION OF TWO INCOMING STREAMS IN A DUEL-COMBUSTION RAMJET COMBUSTOR |
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Beijing University of Aeronautics and Astronautics
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| Abstract: |
| This paper describes the physico-mathematical model for entrance flow in a dual combustion ramjet.Combustor and the numerical calculation method for solving the flow field by using Eular equations, also discusses the preliminary result of computation. |
| Key words: Subsonic combustion Supersonic combustion Air flow Assignment Numerical solution |
