A experiment model of S shaped 2D nozzle was designed based on axisymmetric exhaust system and studied on the infrared characteristic experiment rig. Flow parameters and the far field infrared radiation characteristics of the experiment model were measured under experimental conditions
and compared with the baseline axisymmetric nozzle experiment data. Results showed that
infrared radiation power of S shaped 2D nozzle was mainly in the upper detection plane
and the maximum radiation was in 15 degrees
due to the largest radiation contribution of solid walls in this direction angle. Infrared radiation power in lower and side detection plane was much less than that in upper detection plane because of the shielding effect of S shaped 2D nozzle. Compared with the axisymmetric nozzle
S shaped 2D nozzle had significant effect of infrared suppression
the infrared signature of the S shaped 2D nozzle reduced by 81% in the rear direction
and the maximum radiation intensity reduced by 47%
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Related Author
LIU Chang-chun
JI Hong-hu
HUANG Wei
YANG Fang-fang
WU Bo
ZHANG Jing-zhou
SHAN Yong
SHAO Wan-ren
Related Institution
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
先进航空发动机协同创新中心
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
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing Univerisity of Aeronautics and Astronautics