Efficient utilization of heat sink of hydrocarbon fuel for regeneratively cooled scramjet

被引:87
作者
Bao, Wen [1 ]
Li, Xianling [1 ]
Qin, Jiang [1 ]
Zhou, Weixing [1 ]
Yu, Daren [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China
关键词
Heat sink; Hydrocarbon fuel; Chemical reaction; Heat transfer; Scramjet; C-10-C-14; NORMAL-ALKANES; AVIATION KEROSENE; SUPERCRITICAL CONDITIONS; THERMAL-DECOMPOSITION; PRODUCT DISTRIBUTIONS; PROPULSION; CRACKING;
D O I
10.1016/j.applthermaleng.2011.09.036
中图分类号
O414.1 [热力学];
学科分类号
摘要
Heat sink (cooling capacity) of limited hydrocarbon fuel is not rich for the regenerative cooling of scramjet. It is therefore very important to use the heat sink of fuel efficiently. This paper focuses on the effect of operating conditions of cooling system on the heat sink use of hydrocarbon fuel. Considering the coupling among flow, heat transfer and chemical reaction, a one-dimensional model is developed to evaluate the heat sink use of endothermic hydrocarbon fuel. The model is validated by comparing the calculated results with the experimental data measured through an electrical heating flow reactor, in which thermal cracking takes place for n-decane. Using the developed model, the effect of maximum allowable temperature of metal wall material, flow velocity and uneven heat flux distribution of scramjet has been evaluated by simulating some typical operating conditions, and some conclusions are drawn to assist the fundamental understanding of heat sink use of endothermic hydrocarbon fuel. It is believed that the present investigation will provide a useful reference for the design of cooling system of scramjet. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:208 / 218
页数:11
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