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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. |
| 关键词: 火箭发动机喷管 等熵流 特性线法 |
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| PREDICTION OF TWO-DIMENSIONAL SUPERSONIC NOZZLE FLOW FIELD |
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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. |
| Key words: Rocket engine nozzle Isentropic flow Characteristic method |
