| 引用本文: | 谭建国,陈小前,杨涛,等.燃烧对固体燃料冲压发动机附着点的影响.[J].国防科技大学学报,2000,22(2):29-32.[点击复制] |
| TAN Jianguo,CHEN Xiaoqian,YANG Tao,et al.Combustion Effect on the Reattachment Point in Solid Fuel Ramjet[J].Journal of National University of Defense Technology,2000,22(2):29-32[点击复制] |
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| 燃烧对固体燃料冲压发动机附着点的影响 |
| 谭建国, 陈小前, 杨涛, 张为华 |
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(国防科技大学 航天与材料工程学院 湖南 长沙 410073)
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| 摘要: |
| 应用PHOENICS软件模拟了固体燃料冲压发动机(SFRJ)的冷流和以HTPB、PS为推进剂的简单反应流。结果表明:在相同入口条件下,燃烧使附着点明显前移,从而改变了流场结构;入口温度不影响冷流时的附着点,但在有反应情况下则有一定影响;在两种情况下入口流量对附着点均无影响。 |
| 关键词: 固体燃料冲压发动机 附着点 内流场 数值模拟 |
| DOI： |
| 投稿日期：1999-09-05 |
| 基金项目:国家自然科学基金资助项目 |
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| Combustion Effect on the Reattachment Point in Solid Fuel Ramjet |
| TAN Jianguo, CHEN Xiaoqian, YANG Tao, ZHANG Weihua |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073 China)
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| Abstract: |
| Cold flow field and simple-reaction flow field of the combustion of HTPB and PS within the solid fuel ramjet (SFRJ) are simulated using PHOENICS program. The result shows that the reattachment point moves forward so that the flow field structure is altered in case of combustion. In case of cold flow, the reattachment point doesn't change with inlet temperature, but it does so in simple-reaction flow field. And it doesn't change with inlet mass flux in both conditions. |
| Keywords: Solid fuel ramjet Reattachment point Internal flow field Numerical simulation |
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