| 二维等熵喷管流场计算 |
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| 引用本文： | 方国尧.二维等熵喷管流场计算[J].推进技术,1988,9(3):6-11,73. |
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| 作者姓名： | 方国尧 |
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| 摘 要： | 本文介绍了用于计算超音速火箭喷管特性线方法.从基本原理、几个问题的处理到计算结果的分析和处理,得到某些有益的结果,可供喷管设计和喷管受热分析参考.
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| 关 键 词： | 火箭发动机喷管 等熵流 特性线法 |
PREDICTION OF TWO-DIMENSIONAL SUPERSONIC NOZZLE FLOW FIELD |
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| Fang Guoyao.PREDICTION OF TWO-DIMENSIONAL SUPERSONIC NOZZLE FLOW FIELD[J].Journal of Propulsion Technology,1988,9(3):6-11,73. |
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| Authors: | Fang Guoyao |
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| Institution: | Fang Guoyao |
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| Abstract: | This paper presents a method of two-dimensional characteristic which can be applied to the calculation and design of a rocket supersonic nozzle.Some useful conclusions are drawn from the analysis of computational results.The results,brought about by the method are so good that the method can be suggested as a reference for nozzle design and heat transfer analysis of rocket nozzle. |
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| Keywords: | Rocket engine nozzle Isentropic flow Characteristic method |
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