机译:承受冲击射流的微型针状鳍片的传热增强
Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY 12180, USA,Department of Chemical Engineering, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139-4307, USA;
Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY 12180, USA;
Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY 12180, USA;
Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY 12180, USA;
heat transfer; jet impingement; micro pin fins; electronics cooling;
机译:在横流条件下,通过在横流条件下将Al_2O_3水纳米流体的喷射引起的热传递增强 - 一个数值研究
机译:通过微针翅片表面的射流撞击增强流沸腾传热
机译:针鳍形状和构型对微型针鳍射流冲击的单相传热特性的影响
机译:微型针状翅片对射流阵列撞击传热的影响:射流到目标距离,微型针状翅片形状,高度和雷诺数的影响
机译:紧凑型换热器技术的补充:金属泡沫翅片中的射流冲击冷却,流动和热传递。
机译:TiO2纳米溶液浓度对加热铝板双撞击射流传热增强的影响
机译:共轭空气射流冲击翅片式散热器的强化传热特性
机译:用于先进涡轮发动机部件的microfog润滑剂应用系统,第2阶段。任务3,4和5微流体喷射器的润湿性和传热冲击加热旋转盘,并评估重新分级喷嘴和涡流雾发生器