Numerical research on infrared radiation characteristics of two-dimension nozzle with shelter covering
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Numerical research on infrared radiation characteristics of two-dimension nozzle with shelter covering
Vol. 26, Issue 10, (2011)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国航空工业集团公司 沈阳发动机设计研究所,沈阳,110015
作者简介:
基金信息:
DOI:
CLC:
Published:2011
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WU Bo, ZHANG Jing-zhou, SHAN Yong, et al. Numerical research on infrared radiation characteristics of two-dimension nozzle with shelter covering[J]. 2011, 26(10).
DOI:
WU Bo, ZHANG Jing-zhou, SHAN Yong, et al. Numerical research on infrared radiation characteristics of two-dimension nozzle with shelter covering[J]. 2011, 26(10).DOI:
Numerical research on infrared radiation characteristics of two-dimension nozzle with shelter covering
Based on CFD/IR(computational fluid dynamics/infrared radiation) numerical calculations
the effects of shelter covering fixed at nozzle trailing edge and cooling air injected inside the shelter covering passage on infrared radiation characteristics of turbofan engine two-dimensional nozzle with aspect ratio 3.33 were investigated.The results based on the present parameters show that
ejected or forced cooling air flow through shelter covering passage enhances further mixing with plume
and suppresses plume infrared radiation in comparison with pure two-dimensional nozzle.As the cooling air massflow increases
the cooling action on nozzle trailing edge is more obvious.Utilizing nozzle ejection effectively could achieve satisfactory infrared radiation suppression.The suppression action on nozzle total infrared radiation with shelter covering is only realized in the detecting azimuth where the infrared radiation from nozzle inner walls is predominant.
Experiment on infrared radiation characteristics of S shaped 2D nozzle
Numerical simulation on infrared radiation characteristics of serpentine 2-D 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
Experiment on infrared signature of two dimensional convergent-divergent vectoring nozzle exhaust system
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Related Institution
南京航空航天大学 能源与动力学院
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 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