| 扰流柱几何参数对层板流阻和换热特性的影响 |
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| 引用本文： | 袁星,吕东.扰流柱几何参数对层板流阻和换热特性的影响[J].航空动力学报,2009,24(5):1016-1021. |
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| 作者姓名： | 袁星 吕东 |
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| 作者单位： | 1. 北京航空航天大学,能源与动力工程学院,航空发动机气动热力重点实验室,北京,100191
2. 中国航空工业集团公司,沈阳发动机设计研究所,沈阳,110015 |
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| 摘 要： | 研究了扰流柱几何参数中填充比和直径比对于层板结构流阻和换热特性的影响,在进口流量和两侧换热条件相同情况下,对孔径、通道高度和开孔率相同,扰流柱均为圆柱形,出气孔均倾斜60°角,但扰流柱填充比和扰流柱直径比不一样的15种模型进行了流固耦合计算,得到了模型的流阻和换热特性.结果表明对于流阻而言,填充比的增加有利于层板模型流阻的减小和换热效率的提高;同时,在等填充比条件下,主扰流柱直径的增加有利于层板流阻的减小;当主、副扰流柱直径相同时,换热效果达到最佳.
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| 关 键 词： | 层板 填充比 直径比 流阻系数 换热效率 数值模拟 |
| 收稿时间： | 2008/12/2 0:00:00 |
| 修稿时间： | 5/7/2009 12:00:00 AM |
Effects of pin-fin's geometry parameters on flow resistance and heat transfer characteristics of lamilloy |
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| YUAN Xing and LV Dong.Effects of pin-fin''s geometry parameters on flow resistance and heat transfer characteristics of lamilloy[J].Journal of Aerospace Power,2009,24(5):1016-1021. |
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| Authors: | YUAN Xing and LV Dong |
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| Institution: | 1.National Key Laboratory on Aero-Engines;School of Jet Propulsion;Beijing University of Aeronautics and Astronautics;Beijing 100191;China;2.Shenyang Aero-Engine Research Institute;Aviation Industry Corporation of China;Shenyang 110015;China |
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| Abstract: | This paper dealt with a numerical simulation of the flow resistance and heat transfer characteristics on fifteen different laminated porous wall models.The effects of pin-fin's fill ratio and diameter ratio were investigated.This investigation considered fifteen geometry models: pin-fin's fill ratio and diameter ratio were varied from 0.15 to 0.35 or from 0.3 to 0.7 respectively,while pin-fin's fill ratio was kept at 0.25.Length and height of the whole model were 4 mm and 2 mm respectively;height of pin-fin... |
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| Keywords: | lamilloy fill ratio diameter ratio flow resistance coefficient heat transfer efficiency numerical simulation |
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