DocumentCode :
175783
Title :
Research on measurement of infrared spectral radiant intensity of aero-engine exhaust system
Author :
Yanmei Liu ; Li Fu ; Jianhui Xi ; Yan Ren
Author_Institution :
Shenyang Aerosp. Univ., Shenyang, China
fYear :
2014
fDate :
May 31 2014-June 2 2014
Firstpage :
1177
Lastpage :
1180
Abstract :
This paper presents a testing method for infrared radiation characteristics of the aircraft exhaust system. By using graphical programming language of virtual instrument development testing platform, infrared radiation characteristics of jet aircraft are studied. Infrared radiation can be achieved, displayed and so on. The virtual panel and block diagram are designed. The system designed mainly is composed of infrared radiometer calibration, data collection procedures and showing procedures. Simulation results show that the method is reliable and practical.
Keywords :
aerospace computing; aircraft instrumentation; infrared spectra; jet engines; mechanical engineering computing; radiometry; virtual instrumentation; visual languages; aero-engine exhaust system; aircraft exhaust system; block diagram; data collection procedures; graphical programming language; infrared radiometer calibration; infrared spectral radiant intensity measurement; jet aircraft; showing procedures; testing method; virtual instrument development testing platform; virtual panel; Aircraft; Calibration; Exhaust systems; Instruments; Missiles; Radiometry; Testing; calibration; infrared radiation; testing platform; virtual panel;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location :
Changsha
Print_ISBN :
978-1-4799-3707-3
Type :
conf
DOI :
10.1109/CCDC.2014.6852344
Filename :
6852344
Link To Document :
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