Calculation and Simulation on Infrared Radiation of Hot Jet from Engine

被引：3
|
作者：
Li Jian-xun [1 ]
Tong Zhong-xiang [1 ]
Wang Chao-zhe [1 ]
Tong Qi [1 ]
Li He [1 ]
Zhang Zhi-bo [1 ]
机构：
[1] AF Engn Univ, Aeronaut & Astronaut Engn Inst, Xian 710038, Peoples R China
来源：
SPECTROSCOPY AND SPECTRAL ANALYSIS | 2013年 / 33卷 / 01期
关键词：
Thermotics; Engine; Infrared radiation; Hot jet; Infrared image;
D O I：
10.3964/j.issn.1000-0593(2013)01-0007-07
中图分类号：
O433 [光谱学];
学科分类号：
0703 ; 070302 ;
摘要：
Spectral distribution of infrared radiation from plume by the method to calculate infrared radiance of the gaze direction in small sight field was calculated. Based on numerical value and form of radiative transfer equation, infrared radiant intensity of the gaze direction was calculated using the Malkmus statistical narrow-band model and CG approach. Flow field and mole fraction distribution were simulated using a FLUENT computational fluid dynamic (CFD) software. Infrared imaging simulation model of hot jet was established. The hot jet's infrared images of liquid rocket engine were generated. The results demonstrate that the method can detect well-resolved fine structure of flow field. And the model is also applicable to calculation and simulation on infrared radiation of hot jet from engine.
引用
收藏
页码：7 / 13
页数：7
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