Thermal Cracking of Endothermic Hydrocarbon Fuel in Regenerative Cooling Channels with Different Geometric Structures

2018 ◽  
Vol 32 (6) ◽  
pp. 6524-6534 ◽  
Author(s):  
Fuqiang Li ◽  
Zaizheng Li ◽  
Kai Jing ◽  
Li Wang ◽  
Xiangwen Zhang ◽  
...  
2020 ◽  
Vol 142 (11) ◽  
Author(s):  
Xin Li ◽  
Silong Zhang ◽  
Jiang Qin ◽  
Wen Bao

Abstract Microrib is regarded as an efficient method to regulate the heat transfer and thermal cracking of hydrocarbon fuel in regenerative cooling channels of advanced aero-engines. In order to explore the regulation mechanism of microribs on heat transfer of endothermic hydrocarbon fuel with thermal cracking in the unilateral heated channels, a three-dimensional simulation model including a 22-step cracking mechanism was built and experimentally tested. Besides, a macroscopic approach based on time scale analysis is proposed to estimate effects of obstacles on turbulence and thermal cracking. The studies demonstrated that due to unilateral heating, the regulation of microribs on heat transfer and thermal cracking is nonuniform in the channel, relating to local turbulence intensity and fluid properties. Particularly, the thermal cracking of fuel responses more slowly than turbulence when meeting obstacles. In this case, the regulation of microribs on the heat transfer characteristics of cracking hydrocarbon fuel is dominated by the direct perturbation of microribs on flow momentum, not through promoting chemical absorption of thermal cracking by microribs. Furthermore, higher fuel conversion and higher fluid temperature both assist the promotion of microribs on thermal cracking to a limited extent but has little effect on the acceleration of microribs on local turbulent flow.


2011 ◽  
Vol 56 (6) ◽  
pp. 2980-2986 ◽  
Author(s):  
H. W. Deng ◽  
C. B. Zhang ◽  
G. Q. Xu ◽  
Z. Tao ◽  
B. Zhang ◽  
...  

2021 ◽  
pp. 1-24
Author(s):  
Hui-Sheng Peng ◽  
Bei-Jing Zhong

Abstract Chemical kinetic mechanism plays a vital role in the deep learning of reacting flow in practical combustors, which can help obtain many details of the combustion process. In this paper, a surrogate model and a skeletal mechanism for an endothermic hydrocarbon fuel were developed for further investigations of the combustion performance in hypersonic vehicles: (1) The surrogate model consists of 81.3 mol% decalin and 18.7 mol% n-dodecane, which were determined by both the composition distributions and key properties of the target endothermic hydrocarbon fuel. (2) A skeletal kinetic mechanism only containing 56 species and 283 reactions was developed by the method of “core mechanism​ sub mechanism”. This mechanism can be conveniently applied to the simulation of practical combustors for its affordable scale. (3) Accuracies of the surrogate model and the mechanism were systematically validated by the various properties of the target fuel under pressures of 1-20atm, temperatures of 400-1250K, and equivalence ratios of 0.5-1.5. The overall errors for the ignition and combustion properties are no more than 0.4 and 0.1, respectively. (4) Laminar flame speeds of the target fuel and the surrogate model fuel were also measured for the validations. Results show that both the surrogate model and the mechanism can well predict the properties of the target fuel. The mechanism developed in this work is valuable to the further design and optimization of the propulsion systems.


2022 ◽  
Author(s):  
William A. Mullin ◽  
Keaton Melendez ◽  
Benjamin Stefanko ◽  
Aaron Bell ◽  
Grant Davis ◽  
...  

2021 ◽  
Vol 143 (2) ◽  
Author(s):  
Zekun Zheng ◽  
Xinyan Pei ◽  
Siqian Yan ◽  
Lingyun Hou

Abstract Liquid-fuel regenerative cooling is a promising turbine cooling technology. We developed a numerical model of heat transfer coupled with oxidation deposition in a rotatory channel for regenerative cooling applications. Source terms for the centrifugal and Coriolis forces caused by rotation were added to the momentum equations and turbulent transport equations. A kinetic model for the thermal oxidation and deposition of supercritical hydrocarbon fuel was used to predict the oxidation deposition process. Coupled fluid–solid simulations of the heat transfer and oxidation deposition of hydrocarbon fuel in a U-shaped channel at five rotation numbers showed that the rotation improves convective heat transfer in the cooling channel and prevents the occurrence of a heat transfer deterioration zone. The average deposition rate in the channel decreased with increasing rotation number. In the centrifugal section of the rotatory channel, the Coriolis force caused the temperatures of the leading wall to be higher than those of the trailing wall, but the differences became smaller and nearly disappeared in the elbow and centripetal sections. The deposition rate on the leading wall was higher than that on the trailing wall in the straight centrifugal channel. In the bending section, the oxidation deposits were more prone to form on the inner edge than on the outer edge.


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