机译:基于矢量双合成射流致动器的撞击流场和传热特性
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, People's Republic of China;
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, People's Republic of China;
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, People's Republic of China;
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, People's Republic of China;
College of Mechatronics and Control Engineering, Shenzheng University, Shenzheng 518060, People's Republic of China;
Vectoring dual synthetic jet; Sweeping-flow capability; Large-area electronic cooling; Heat-transfer influence domain;
机译:压电致动器驱动的合成射流冲击下的流动和传热特性
机译:带有三角形翼片和合成射流的组合装置的射流的传热和流体流动特性
机译:双合成射流流动调节和冲击传热的实验研究
机译:射流与壁间距对热硅上湍流射流喷嘴的传热特性和流场的影响
机译:平板表面干燥过程中冲击空气射流流动和传热特性的数值模拟
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:圆形撞击喷射的流动和传热特性添加环形抽吸流动。将撞击壁放置在自由射流的潜在核心区域中的情况。
机译:撞击射流阵列内的传热特性。横流温度对射流温度的影响