Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning
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Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning
Vol. 22, Issue 10, (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:
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LUO Ming-dong, JI Hong-hu, HUANG Wei. Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning[J]. 2007, 22(10).
DOI:
LUO Ming-dong, JI Hong-hu, HUANG Wei. Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning[J]. 2007, 22(10).DOI:
Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning
The numerical calculation method of infrared radiant intensity of exhaust system of turbine engine without afterburning was studied.Due consideration was given to emission and reflection of solid wall
absorption and emission of water vapor
carbon dioxide and carbon monoxide in the gas.This method was used to calculate the infrared radiant intensity of a scaled model of turbofan exhaust system
and compare with the experimental results.These results show that
this method could help you calculate accurately the infrared radiant intensity of turbine engine at waveband of 35μm
Numerical simulation of infrared radiation characteristics for exhaust system of an UAV with engine installed on the back of the fuselage
Research on measurement method of mid-IR spectral radiant intensity of exhaust system with FTIR spectrometer
Experiment on infrared radiation characteristics of S shaped 2D nozzle
Experiment on infrared signature of a model of serpentine twodimensional exhaust system
Investigation on aerodynamic and infrared characteristics of spherical convergent two-dimensional vectoring nozzle: simulating ground status
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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