| Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors |
| Li F(李飞); Yu XL(余西龙); Gu HB(顾洪斌); Li Z(李智); Zhao Y; Ma L; Chen LH(陈立红); Zhang XY(张新宇); Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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发表期刊 | Applied Optics
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| 2011
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卷号 | 50期号:36页码:6697-6707 |
ISSN | 1559-128X
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摘要 | This paper reports the simultaneous measurements of multiple flow parameters in a scramjet facility operating at a nominal Mach number of 2.5 using a sensing system based on tunable diode-laser absorption spectroscopy (TDLAS). The TDLAS system measures velocity, temperature, and water vapor partial pressure at three different locations of the scramjet: the inlet, the combustion region near the flame stabilization cavity, and the exit of the combustor. These measurements enable the determination of the variation of the Mach number and the combustion mode in the scramjet engine, which are critical for evaluating the combustion efficiency and optimizing engine performance. The results obtained in this work clearly demonstrated the applicability of TDLAS sensors in harsh and high-speed environments. The TDLAS system, due to its unique virtues, is expected to play an important role in the development of scramjet engines. (C) 2011 Optical Society of America |
关键词 | Absorption-spectroscopy
Water-vapor
Temperature Distributions
Gas Temperature
Combustion
Cavity
Operation
Engines
Model
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学科领域 | Optics
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DOI | 10.1364/AO.50.006697
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URL | 查看原文
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收录类别 | SCI
; EI
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语种 | 英语
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WOS记录号 | WOS:000299166700020
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关键词[WOS] | ABSORPTION-SPECTROSCOPY
; WATER-VAPOR
; TEMPERATURE DISTRIBUTIONS
; GAS TEMPERATURE
; COMBUSTION
; CAVITY
; OPERATION
; ENGINES
; MODEL
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WOS研究方向 | Optics
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WOS类目 | Optics
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项目资助者 | The work is partially supported by National Natural Science Foundation of China (Grant Nos. 90816015 and 11002148). The authors acknowledge the technical assistance provided by the technicians D. H. Song and Z. M. Luo at the Institute of Mechanics, Chinese Academy of Sciences.
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课题组名称 | LHD高温气流激光诊断
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论文分区 | 二类
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引用统计 |
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文献类型 | 期刊论文
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条目标识符 | http://dspace.imech.ac.cn/handle/311007/45163
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专题 | 高温气体动力学国家重点实验室
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通讯作者 | Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China |
推荐引用方式 GB/T 7714 |
Li F,Yu XL,Gu HB,et al. Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors[J]. Applied Optics,2011,50,36,:6697-6707.
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APA |
李飞.,余西龙.,顾洪斌.,李智.,Zhao Y.,...&Yu, XL .(2011).Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors.Applied Optics,50(36),6697-6707.
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MLA |
李飞,et al."Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors".Applied Optics 50.36(2011):6697-6707.
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