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博士生导师

硕士生导师

任职 : 国家重大专项专家组成员、教育部热防护专业组组长、国际华人计算力学协会理事、中国航空学会理事、中国航空学会强度与设计专业委员会委员、国际边界单元法协会会员、教育部高等学校航空航天类专业教学指导委员会委员

性别:男

毕业院校:Glasgow University

学位:博士

所在单位:力学与航空航天学院

办公地点:海宇楼403A

联系方式:0411-84706332

电子邮箱:xwgao@dlut.edu.cn

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Boundary effects on flow oscillations in transient heat transfer of n-decane at supercritical pressure

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论文类型:期刊论文

发表时间:2018-08-01

发表刊物:INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER

收录刊物:SCIE、EI

卷号:123

页面范围:821-825

ISSN号:0017-9310

关键字:Regenerative cooling; Hydrocarbon fuel; Transient response; Thermoacoustic wave; Pressure oscillation

摘要:A numerical study has been conducted to analyze boundary effects, including different inlet boundary conditions and different inlet section lengths (distances from the inlet boundary to the heated section), on flow dynamics in transient supercritical-pressure heat transfer of n-decane in a circular tube. As the inlet boundary condition changes from a constant flow velocity to a constant stagnation pressure, the pressure oscillation frequency is nearly doubled, and the thermoacoustic wave is in the first longitudinal mode. The frequency of mass flow rate oscillation is essentially the same as that of the pressure wave. Different inlet boundary conditions exert no effect on the pressure wave amplitude but make strong influence on the amplitude of mass flow rate oscillation at the outlet of the heated section. As the inlet insulation section length increases under a constant inlet stagnation pressure, frequencies of both pressure and mass flow rate oscillations proportionally decrease, and the thermoacoustic waves remain in the first longitudinal mode. Different inlet section lengths appear to make only minor effect on the amplitudes of both pressure and mass flow rate oscillations at the outlet of the heated section, and the maximum amplitude in each wave is around 10% of its steady-state value. (C) 2018 Elsevier Ltd. All rights reserved.