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Detailed heat transfer investigation of an impingement jet array with large jet-to-jet distance

机译:具有大型喷射距离的冲击喷射阵列的详细传热研究

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摘要

The heat transfer performance of a large jet-to-jet distance impingement configuration with a jet-to-jet spacing X/D = Y/D = 10 was experimentally studied for turbomachinery applications. Narrowband thermochromic liquid crystals (TLCs) were used to record the target wall temperature. Pressure taps were set along the experimental rig to measure the pressure loss. Improved measurement methods with multiple TLCs and a ramp heater were studied. The work was done for different Reynolds numbers (Re = 15,000-35,000), different jet to target plate distances (H/D = 3-5) and different cross-flow schemes. The results from the improved methods show good agreement with the basic measurement method. It confirms that the single TLC, step heater method is sufficient for the current experimental study. The improved methods are confirmed to be reliable and are suitable for complex applications with extremely large heat transfer variations over the measured surface, or extremely high local heat transfer coefficients. Experimental results indicate that a smaller jet to target plate distance and a smaller cross-flow scheme can provide a better heat transfer performance in the studied range. When compared to the impingement configuration with X/D = Y/D = 5, the results show that a larger jet-to-jet distance configuration provides a higher overall heat transfer when the mass flow rate is kept constant.
机译:使用喷射到喷射间隔X / D = Y / D = 10的大型喷射距离冲击配置的传热性能进行了实验研究涡轮机应用。使用窄带热致铬液晶(TLC)用于记录目标壁温。沿着实验钻机设定了压力点心以测量压力损失。研究了具有多个TLC和斜坡加热器的改进的测量方法。这项工作是针对不同的雷诺数(RE = 15,000-35,000),不同的射流到目标板距离(H / D = 3-5)和不同的横流方案。改进方法的结果与基本测量方法展示了良好的一致性。它证实单个TLC,步骤加热方法足以用于当前的实验研究。确认改进的方法是可靠的,适用于在测量的表面上具有极大的传热变化的复杂应用,或极高的局部传热系数。实验结果表明,较小的射流到靶板距离和较小的横流方案可以在研究范围内提供更好的传热性能。与X / D = Y / D = 5的冲击配置相比,结果表明,当质量流量保持恒定时,更大的喷射距离配置提供更高的总热传热。

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