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亚燃、超燃双重燃烧进气分流数值模拟研究 |
马继华, 丁家喜
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北京航空航天大学
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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 |
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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 |
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