推进技术 ›› 1991, Vol. 12 ›› Issue (3): 54-61.
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马继华,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.
关键词: 亚音速燃烧;超音速燃烧;空气流;分配;数值解
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
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.
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