参考焓值法在高速槽道湍流中的修正 | |
Alternative Title | THE OPTIMIZED REFERENCE ENTHALPY METHOD USING IN HIGH-SPEED TURBULENT CHANNEL FLOWS |
陈小平; 李新亮; 仲峰泉 | |
Source Publication | 力学学报 |
2013-07-23 | |
Volume | 45Issue:4Pages:614-618 |
ISSN | 0459-1879 |
Abstract | 利用高来流马赫数为3, 5, 6, 7, 10的槽道湍流直接数值模拟(direct numerical simulations, DNS)数据, 评估和修正经典的参考焓值法. 研究表明在高来流马赫数槽道湍流中, 经典参考焓值法预测的壁面热流与DNS结果相差很大, 需要作适当的修正.修正参考焓值法Ⅰ和Ⅱ的预测结果明显优于经典参考焓值法;并且修正参考焓值法Ⅱ更加适用于高马赫数流动, 其壁面热流与DNS结果的相对误差在10%以内. 同时, 修正参考焓值法Ⅱ的普适性在超声速燃烧室隔离段热环境试验中得到了验证. |
Other Abstract | Direct numerical simulations of high-speed turbulent channel flows have been performed. The classic reference enthalpy method was evaluated and optimized by using the data with inflow Mach numbers of 3, 5, 6, 7, and 10. In fully developed turbulent flow, studies have shown that the classic reference enthalpy method is not applicable in high-speed channel flows. The wall heat flux predicted by the optimized reference enthalpy methods I and II are much better than the classic reference enthalpy method; moreover, the optimized reference enthalpy method II is more suitable, whose errors are within 10% compared with DNS. At the same time, the optimized reference enthalpy method II has been verified based on the experiment data of thermal environment of supersonic combustor. |
Keyword | 高超声速飞行 槽道湍流 直接数值模拟 参考焓值法 |
Subject Area | 流体力学 ; 湍流 ; 空气动力学 |
URL | 查看原文 |
Indexed By | EI ; CSCD |
Language | 中文 |
Funding Organization | 国家自然科学基金项目(11072248), 国家重大基础研究发展规划项目(2009CB724100),国家高技术研究发展计划项目(2012AA01A304) 和中国科学院知识创新工程项目(KJCX2-EW-J01) 资助 |
CSCD ID | CSCD:4888140 |
Department | LHD可压缩湍流 |
Classification | 二类 |
Citation statistics | |
Document Type | 期刊论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/47366 |
Collection | 高温气体动力学国家重点实验室 |
Corresponding Author | 李新亮 |
Recommended Citation GB/T 7714 | 陈小平,李新亮,仲峰泉. 参考焓值法在高速槽道湍流中的修正[J]. 力学学报,2013,45,4,:614-618. |
APA | 陈小平,李新亮,&仲峰泉.(2013).参考焓值法在高速槽道湍流中的修正.力学学报,45(4),614-618. |
MLA | 陈小平,et al."参考焓值法在高速槽道湍流中的修正".力学学报 45.4(2013):614-618. |
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