| 摘要: |
| 在喷管喉部后方注水，使喷喉临界状态在一定范围内不随出口环境的压力而变化，并对其流动特性进行了分析。在一维定常流动假设的基础上，采用控制容积法建模，在一定参数范围内选代计算喷管背压、喷水量与喷管几何参数之间的数值关系，并对计算结果进行分析和讨论。 |
| 关键词: 鱼雷发射 涡轮机 喷管气流 加质流 |
| DOI： |
| 分类号:TJ630.32 |
| 基金项目: |
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| AN ANALYSIS ON FLOW IN CONVERGING-DIVERGING NOZZLE WITH WATER ADDITION |
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Pan Hongliang, Zhao Lianfeng
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Coll.of Marine Engineering, Northwestern Polytechnical Uniu.,Xi’an,710072
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| Abstract: |
| The general features of flow in converging-diverging nozzle with water addition areinvestigated. water is injected at down stream of the throat in order to keep throat critical when theback pressure is changed. With control-volume methane a model is developed under the assumption ofsteady one-dimensionnal and numerical solution is obtained. |
| Key words: Torpedo launching Turbine engine Nozzle gas flow Flow with mass addition |
