IMECH-IR  > 高温气体动力学国家重点实验室
超临界压力下航空煤油流动与传热特性试验
Alternative TitleExperiment on convective heat transfer of aviation kerosene under supercritical pressures
江晨曦; 仲峰泉; 范学军; 俞刚
Source Publication推进技术
2010-04-15
Volume31Issue:2Pages:230-234
Abstract本文针对超燃冲压发动机再生冷却系统运行条件,实验研究了大庆RP-3煤油在超临界压力下的流动和传热特性,目的在于研究煤油在各种工况下的流动参数变化以及对流传热规律. 煤油通过二级煤油加热/输运系统加热,试验的煤油压力约2.6M~5.0MPa,油温约300~800 K. 相应的壁面热流密度为10~300 kW/m2. 通过油温与壁温的同步测量,结合非定常传热分析,获得了超临界压力下、亚/超临界温度范围内煤油的流动和传热物理参量的变化曲线
Keyword航空煤油 超临界态 对流传热
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Indexed ByEI ; CSCD
Language中文
Funding Organization国家自然科学基金项目(10672169 ; 10742003 ; 10621202)
CSCD IDCSCD:3950789
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43888
Collection高温气体动力学国家重点实验室
Corresponding Author江晨曦
Recommended Citation
GB/T 7714
江晨曦,仲峰泉,范学军,等. 超临界压力下航空煤油流动与传热特性试验[J]. 推进技术,2010,31(2):230-234.
APA 江晨曦,仲峰泉,范学军,&俞刚.(2010).超临界压力下航空煤油流动与传热特性试验.推进技术,31(2),230-234.
MLA 江晨曦,et al."超临界压力下航空煤油流动与传热特性试验".推进技术 31.2(2010):230-234.
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