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Heat transfer and flow field measurements of a pulsating round jet impinging on a flat heated surface

机译:撞击在加热平面上的脉动圆形射流的传热和流场测量

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Heat transfer and flow field characteristics of a pulsating round air jet, impinging on a flat heated target surface were measured and compared to those of a steady impinging jet. The jet was partially confined and the target surface stand-off distance equaled two nozzle diameters, D. Investigated Reynolds numbers ranged from Re = 4,606 to 13,513, while pulsating jet velocities varied nearly sinusoidal with Strouhal numbers ranging between 2x 10(-3) Sr 15.6 x 10(-3). Results indicated that besides the well-known secondary Nusselt number peak at approximately 2D from the stagnation point, an additional distinct increase in Nusselt number was detected at approximately 4D from the stagnation point as a result of partial jet confinement. For the studied Re and Sr-number range, jet pulsation resulted in both enhanced and slightly reduced overall heat transfer. Our results indicated that the physical mechanism responsible for overall heat transfer enhancement or reduction due to jet pulsation is increased or reduced primary vortex generation Strouhal numbers (Sr-nu), respectively. The latter were extracted from phase-locked particle image velocimetry measurements. Overall heat transfer modulation linearly depended on the ratio of the ensemble averaged pulsating jet and steady jet primary vortex generation Strouhal numbers, (Sr) over bar (nu)/(Sr) over bar (nu,0). Overall heat transfer enhancement and reduction was obtained when (Sr) over bar (nu)/(Sr) over bar (nu,0) 1 and (Sr) over bar (nu)/(Sr) over bar (nu,0) 1, respectively.
机译:测量了撞击在平坦的加热目标表面上的脉冲圆形空气射流的传热和流场特性,并将其与稳定撞击射流的传热和流场特性进行了比较。射流被部分限制,目标表面的对峙距离等于两个喷嘴直径D。研究的雷诺数范围从Re = 4,606到13,513,而脉动射流速度变化几乎为正弦曲线,斯特劳哈尔数范围在2x 10(-3) Sr <15.6×10(-3)。结果表明,除了众所周知的次级Nusselt峰出现在停滞点大约2D处,由于部分射流限制,在距停滞点大约4D处还发现了Nusselt数的额外明显增加。对于所研究的Re和Sr数范围,射流脉动导致整体传热的提高和略有降低。我们的结果表明,负责整体热传递增强或减少(由于射流脉动)的物理机制分别增加或减少了初级涡流产生的Strouhal数(Sr-nu)。后者是从锁相颗粒图像测速仪的测量中提取的。总的传热调制线性地取决于整体平均脉动射流与稳定射流初级涡流生成Strouhal数之比,(Sr)超过bar(nu)/(Sr)超过bar(nu,0)。当(Sr)超过bar(nu)/(Sr)超过bar(nu,0)>(Sr)超过bar(nu)/(Sr)超过bar(nu,0)时,总传热增强和降低<1。

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