@inproceedings{d68e8e498f294e559602986ce3ec9ada,
title = "Numerical calculation of the radiation heat transfer between rocket motor nozzle's wall and gas",
abstract = "The heat flux density of radiation heat transfer between rocket motor nozzle's wall and gas is one of the most important factors to decide temperature of nozzle's wall. It also provides an invaluable references advice for choosing the material of wall and type of cooling. The numerical calculation based on finite volume method is introduced in the paper. After analysis of the formula of FVM without the influence of scattering, a formula that is used to let spectral radiant intensity that is the calculation of FVM be converted into heat flux density of radiation heat transfer is deduced. It is compiled that the program based on FVM is used to calculate the heat flux density. At the end, the heat flux density of radiation heat transfer of 3D model of double-arc nozzle's wall is calculated under different condition, then simply analysis cooling system is performed.",
keywords = "Finite volume method, Radiation heat transfer, Rocket motor nozzle",
author = "Yipeng Zhou and Dingqiang Zhu",
note = "Publisher Copyright: {\textcopyright} 2014 SPIE.; International Symposium on Optoelectronic Technology and Application 2014: Infrared Technology and Applications, IPTA 2014 ; Conference date: 13-05-2014 Through 15-05-2014",
year = "2014",
doi = "10.1117/12.2070646",
language = "英语",
series = "Proceedings of SPIE - The International Society for Optical Engineering",
publisher = "SPIE",
editor = "Zhichuan Niu and Mircea Guina and Jin Lu and Haimei Gong",
booktitle = "International Symposium on Optoelectronic Technology and Application 2014",
address = "美国",
}