【24h】

NUMERICAL PERFORMANCE of A NOVEL AIR SIDE FIN USED IN HEAVEY DUTY ENGINE

机译:重型发动机用新型空气侧翅片的数值性能

获取原文
获取原文并翻译 | 示例

摘要

In the present study, a 3-D model of a novel air side fin used in heavy duty engine cooling system was established. The fin looks like a wavy fin. There are some upheaval parts in hexagon shape in the air flow direction. A detailed 3-D model which consisted of most geometry information was introduced in CAD software. In numerical simulation model, flow and heat transfer characteristics were analyzed based on energy and momentum governing equations. The detailed geometric parameters which affected air side thermal and flow performance of the novel fin were numerically studied. The Colburn j factor and frictional f factor were calculated according to simulation results. The numerical results showed the upheaval height and upheaval pitch of hexagon shape and fin pitch influenced the fin performance dramatically.
机译:在本研究中,建立了用于重型发动机冷却系统的新型空气侧翅片的3-D模型。鳍看起来像波浪状的鳍。在空气流动方向上有一些六角形的剧变部分。在CAD软件中引入了详细的3-D模型,其中包含大多数几何信息。在数值模拟模型中,基于能量和动量控制方程对流动和传热特性进行了分析。数值研究了影响新型翅片空气侧热和流动性能的详细几何参数。根据仿真结果计算了Colburn j因子和摩擦f因子。数值结果表明,六边形的隆起高度和隆起节距以及翅片节距对翅片性能有显着影响。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号