首页> 外文期刊>Heat transfer >Heat Transfer Enhancement by Using a Rectangular Wing Vortex Generator on the Triangular Shaped Fins of a Plate-Fin Heat Exchanger
【24h】

Heat Transfer Enhancement by Using a Rectangular Wing Vortex Generator on the Triangular Shaped Fins of a Plate-Fin Heat Exchanger

机译:在板翅式换热器的三角形翅片上使用矩形翼型涡旋发生器增强传热

获取原文
获取原文并翻译 | 示例
       

摘要

The present numerical analysis pertains to the heat transfer enhancement in a plate-fin heat exchanger employing triangular shaped fins with a rectangular wing vortex generator on its slant surfaces. The study has been carried out for three different angles of attack of the wing, i.e., 15°, 20° and 26°. The aspect ratio of the wing is not varied with its angle of attack. The flow considered herein is laminar, incompressible, and viscous with the Reynolds number not exceeding 200. The pressure and the velocity components are obtained by solving the continuity and the Navier-Stokes equations by the Marker and Cell method. The present analysis reveals that the use of a rectangular wing vortex generator at an attack angle of 26° results in about a 35% increase in the combined spanwise average Nusselt number as compared to the plate-triangular fin heat exchanger without any vortex generator.
机译:本数值分析涉及板翅式换热器中的传热增强,该板翅式换热器采用三角形翅片在其倾斜表面上具有矩形翼状涡流发生器。已经针对机翼的三个不同的迎角,即15°,20°和26°进行了研究。机翼的长宽比不会随其迎角而变化。本文考虑的流动是层流,不可压缩的且粘性的,雷诺数不超过200。压力和速度分量是通过用Marker和Cell方法求解连续性和Navier-Stokes方程获得的。本分析表明,与没有任何涡流发生器的板式三角形翅片换热器相比,使用矩形翼涡流发生器(攻角为26°)可使组合翼展平均努塞尔特数增加约35%。

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