Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer

LUO Ming-dong; JI Hong-hu; HUANG Wei; CAI Xu; GAO Chao

Chinese

您当前的位置：

首页 >

文章列表页 >

Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer

更新时间：2026-07-07

- Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer
- Vol. 22, Issue 9, (2007)
- 作者机构：
  
  南京航空航天大学能源与动力学院,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2007
- 稿件说明：
移动端阅览
LUO Ming-dong, JI Hong-hu, HUANG Wei, et al. Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer[J]. 2007, 22(9).
DOI：

LUO Ming-dong, JI Hong-hu, HUANG Wei, et al. Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer[J]. 2007, 22(9). DOI：

摘要

通过理论分析及实验研究讨论了傅立叶变换红外(FTIR)光谱仪测量排气系统中红外光谱辐射强度过程中误差产生的原因

设计了一套简易有效的测量方法.用此方法测量了黑体和热喷流的光谱辐射强度.结果表明:该测量方法能够有效地获得排气系统的中红外光谱辐射强度

具有工程实用价值.

Abstract

The reasons of error occurred in measuring Mid-IR spectral radiant intensity of exhaust system with Fourier transform infrared(FTIR) spectrometer was discussed through theoretical analysis and experimental research.A simple and efficient measurement method was also planned to measure the spectral radiant intensity of a blackbody and a hot plume.The results show that Mid-IR spectral radiant intensity of exhaust system could be measured effectively by this method

thus offering a high value of engineering practicability.

关键词

Keywords

references

Views

557

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical simulation of infrared radiation characteristics for exhaust system of an UAV with engine installed on the back of the fuselage

Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning

Experiment on infrared radiation characteristics of S shaped 2D nozzle

Experiment on infrared signature of a model of serpentine twodimensional exhaust system

Investigation on aerodynamic and infrared characteristics of spherical convergent two-dimensional vectoring nozzle: simulating ground status

Related Author

SHI Xiao-juan

刘常春

吉洪湖

王丁

卢浩浩

王浩

季靖远

张靖周

Related Institution

中国航空发动机集团有限公司商用航空发动机有限责任公司

南京航空航天大学能源与动力学院

南京航空航天大学能源与动力学院江苏省航空动力系统重点实验室

先进航空发动机协同创新中心

Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing Univerisity of Aeronautics and Astronautics

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰