Study on Flow and Heat Transfer Characteristics of Supercritical Kerosene in a Round Tube

Feng Gao; Qian Zhang; Hongyu Xiao; Fengli Chen; Xuefeng Xia

doi:10.1051/matecconf/202031603003

All issues

Volume 316 (2020)

MATEC Web Conf., 316 (2020) 03003

References

Open Access

Issue		MATEC Web Conf. Volume 316, 2020 2020 6^th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2020)


Article Number		03003
Number of page(s)		7
Section		Power Machinery Engineering and Application
DOI		https://doi.org/10.1051/matecconf/202031603003
Published online		01 July 2020

Xiao Hongyu. Analysis and Design of Reinforced Active Cooling Structure Reinforcement for Supercombustion Stamping Engine [D]. Xi’an: Master’s Thesis of Air Force Engineering University, 2007 [Google Scholar]
Wang Yingjie. Review of heat transfer characteristics of supercritical fluids[J]. Science & Technology Review, 2012, 30 (33); 74-79 [Google Scholar]
Li Xunfeng, Zhong Fengquan. Numerical study of flow and heat transfer of aviation kerosene tube under supercritical pressure. [J] Propulsion Technology. 2010. Vol.31. No.4 [Google Scholar]
Xianliang Lei, Huixiong Li, Shuiqing Yu, Tingkuan Chen. Numerical investigation on the mixed convection and heat transfer of supercritical water in horizontal tubes in the large specific heat region[J]. Computers and Fluids. 2012, 64, 127-140 [CrossRef] [Google Scholar]
Dong Eok Kim, Moo Hwan Kim. Two layer heat transfer model for supercritical fluid flow in a vertical tube.[J]. The Journal of Supercritical Fluids. 2011, 58 (1), 15-25 [CrossRef] [Google Scholar]
Fan, X J; Yu, G; Li, J G; Lu, X N; Sung. Performan -ce of Supersonic Model Combustors with Distributed Injection of Supercritical Kerosene [R]. AIAA 20075406, 2007 [Google Scholar]
Gong, Les. Real-Time Simulation of Aeroheating of the Hyper-X Airplane [R] NASA. 20110014692, 2011 [Google Scholar]
Guo Chaobang, Li Wenjie, Xing Ya. Research progress on active cooling and high temperature resistant structural components of French supercombustion stamping engines. Aeronautical Missiles, 2011 (11) [Google Scholar]
Ungar, Eugene K.; Schunk, Richard G: Spacecraft Radiator Freeze Protection Using a Regenerative Heat Exchanger [R] NASA 20110012266, 2011 [Google Scholar]
Moholt, Matthew. ARMD Hypersonics Project Materials and Structures: Testing of Scramjet Thermal Protection System Concepts [R]. NASA. 20090012145, 2009 [Google Scholar]

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[1] Xiao Hongyu. Analysis and Design of Reinforced Active Cooling Structure Reinforcement for Supercombustion Stamping Engine [D]. Xi’an: Master’s Thesis of Air Force Engineering University, 2007 [Google Scholar]

[2] Wang Yingjie. Review of heat transfer characteristics of supercritical fluids[J]. Science & Technology Review, 2012, 30 (33); 74-79 [Google Scholar]

[3] Li Xunfeng, Zhong Fengquan. Numerical study of flow and heat transfer of aviation kerosene tube under supercritical pressure. [J] Propulsion Technology. 2010. Vol.31. No.4 [Google Scholar]

[4] Xianliang Lei, Huixiong Li, Shuiqing Yu, Tingkuan Chen. Numerical investigation on the mixed convection and heat transfer of supercritical water in horizontal tubes in the large specific heat region[J]. Computers and Fluids. 2012, 64, 127-140 [CrossRef] [Google Scholar]

[5] Dong Eok Kim, Moo Hwan Kim. Two layer heat transfer model for supercritical fluid flow in a vertical tube.[J]. The Journal of Supercritical Fluids. 2011, 58 (1), 15-25 [CrossRef] [Google Scholar]

[6] Fan, X J; Yu, G; Li, J G; Lu, X N; Sung. Performan -ce of Supersonic Model Combustors with Distributed Injection of Supercritical Kerosene [R]. AIAA 20075406, 2007 [Google Scholar]

[7] Gong, Les. Real-Time Simulation of Aeroheating of the Hyper-X Airplane [R] NASA. 20110014692, 2011 [Google Scholar]

[8] Guo Chaobang, Li Wenjie, Xing Ya. Research progress on active cooling and high temperature resistant structural components of French supercombustion stamping engines. Aeronautical Missiles, 2011 (11) [Google Scholar]

[9] Ungar, Eugene K.; Schunk, Richard G: Spacecraft Radiator Freeze Protection Using a Regenerative Heat Exchanger [R] NASA 20110012266, 2011 [Google Scholar]

[10] Moholt, Matthew. ARMD Hypersonics Project Materials and Structures: Testing of Scramjet Thermal Protection System Concepts [R]. NASA. 20090012145, 2009 [Google Scholar]