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超燃冲压模型发动机实验设备与实验技术
Progress in studies on test facility and experimental technique for model scramjet
查看参考文献43篇
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文摘
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超燃冲压发动机是高超声速飞行器的先进的动力系统，在基础研究和工程应用方面都具有重大意义。其实验设备的建设与实验技术的积累是一个国家在航空航天领域综合实力的体现。本文综述了国外超燃冲压发动机地面实验设备的发展情况，介绍了我国用于超燃冲压模型发动机；实验的高超声速推进实验装置及其关键组成部分的设计思想、研制方法和调试结果。马赫数5.8，总压5MPa，总温2000K，总流量4.5kg/s的设备运行参数为超燃冲压模型发动机的研究提供了必要的实验条件。 |
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其他语种文摘
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Scramjet is an advanced propulsion system for hypersonic vehicles and plays very important roles in both fundamental researches and engineering applications. The construction of the test facilities and the development of the experimental techniques for scramjet investigation signify a national potential in aerospace field. The present paper summarized the development of scramjets and its ground test facilities in the world. It also introduced the first model scramjet test facility in China, called HPTF (Hypersonic Propulsion Test Facility), with the basic considerations and studies in the design and construction of its key elements. The pre-liminary calibration and testing results were also discussed. This facility provides a basic experiment conditions for model scramjet tests with the operational parameters of Mach number of 5.8, total pressure of 5MPa, total temperature of 2000K and total mass flow rate of 4.5kg/s. |
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来源
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力学进展
,2003,33(4):491-498 【核心库】
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关键词
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高超声速推进技术
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地面模拟实验装置
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超燃冲压发动机
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地址
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中国科学院力学研究所, 高温气体动力学重点实验室, 北京, 100080
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语种
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中文 |
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文献类型
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研究性论文 |
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ISSN
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1000-0992 |
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学科
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航天(宇宙航行) |
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基金
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中国科学院“百人计划”项目
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中国科学院大型仪器设备研制项目
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文献收藏号
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CSCD:1166752
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43
共3页
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