| 亚燃、超燃双重燃烧进气分流数值模拟研究 |
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| 引用本文： | 马继华,丁家喜.亚燃、超燃双重燃烧进气分流数值模拟研究[J].推进技术,1991,12(3):54-61,47. |
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| 作者姓名： | 马继华 丁家喜 |
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| 作者单位： | 北京航空航天大学
(马继华)，北京航空航天大学(丁家喜) |
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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.
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| 关 键 词： | 亚音速燃烧 超音速燃烧 数值解 航空发动机 |
NUMERICAL SIMULATION OF TWO INCOMING STREAMS IN A DUEL-COMBUSTION RAMJET COMBUSTOR |
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| Ma Jihua Din Jiaxi.NUMERICAL SIMULATION OF TWO INCOMING STREAMS IN A DUEL-COMBUSTION RAMJET COMBUSTOR[J].Journal of Propulsion Technology,1991,12(3):54-61,47. |
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| Authors: | Ma Jihua Din Jiaxi |
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| Institution: | 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. |
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| Keywords: | Subsonic combustion Supersonic combustion Air flow Assignment Numerical solution |
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