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超燃冲压模型发动机实验设备与实验技术
Alternative TitleProgress in studies on test facility and experimental technique for model scramjet
张新宇; 陈立红; 顾洪斌
Source Publication力学进展
2003
Volume33Issue:4Pages:491-498
ISSN1000-0992
Abstract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。
Keyword高超声速推进技术 地面模拟实验装置 超燃冲压发动机
Subject Area力学
Indexed ByCSCD
Language中文
CSCD IDCSCD:1166752
Citation statistics
Cited Times:8[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/17289
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
张新宇,陈立红,顾洪斌. 超燃冲压模型发动机实验设备与实验技术[J]. 力学进展,2003,33,4,:491-498.
APA 张新宇,陈立红,&顾洪斌.(2003).超燃冲压模型发动机实验设备与实验技术.力学进展,33(4),491-498.
MLA 张新宇,et al."超燃冲压模型发动机实验设备与实验技术".力学进展 33.4(2003):491-498.
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