Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors
Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors
复制标题
带有凹进剪切同轴喷油器的推力室的耦合传热分析
DOI:
10.1016/j.actaastro.2016.12.026
复制
发表时间:
2017
影响因子:
3.5
通讯作者:
Bing
中科院分区:
文献类型:
--
作者:
Jiawen Song;Bing
To investigate the effects of recessed lengths on combustion performance and heat loads in LOX/methane thrust chambers with shear coaxial injectors, a coupled numerical methodology is developed to solve the combustion and heat transfer in thrust chambers with regenerative cooling. In this methodology, the transcritical turbulent combustion is modeled by a validated non-adiabatic flamelet model considering real-fluid properties; turbulent flows within the thrust chamber and cooling channels are computed by a pressure-based coupled algorithm. The validation indicates that the prediction with detailed chemistry mechanism and the Chung method confirms quantitatively to literature experimental data. The results reveal that the recess causes an increase of wall heat flux in the whole thrust chamber and makes the heat flux peak in the combustion chamber moves downstream. Furthermore, both the heat flux peaks in the combustion chamber and nozzle increase first and then decrease as recessed lengths increase. Meanwhile, chamber pressure, hot-gas temperature, and the averaging heat flux of the combustion chamber wall are positively correlated with recessed lengths. However, the heat loads are more sensitive to the recessed lengths than chamber pressure and hot-gas temperature. Much attention should be paid to the protection of chamber wall.
DOI:
--
发表时间:
2009
期刊:
影响因子:
--
作者:
Hideaki Komiyama;Tomokazu Iyoda;Kaori Kamata;込山英秋;Hideaki Komiyama;込山英秋;Hideaki Komiyama;Hideaki Komiyama;Hideaki Komiyama;込山英秋;Hideki Komiyama;Hideki Komiyama;Hideki Komiyama;込山英秋;込山英秋;谷洋海;谷洋海;谷洋海;谷洋海;谷洋海;谷洋海;谷洋海
通讯作者:
谷洋海