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Flow and heat transfer measurements in laminar and turbulent convex surface boundary layers

机译:层流和湍流凸面边界层中的流动和传热测量

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摘要

Convex surface boundary layers have been experimentally investigated in a low speed wind tunnel, in the presence of pressure gradients (k) of-3.6×10~-6≤k≤+3.6×10~-6 for laminar and -3.6×10~-6≤k≤+3.6×10~-6 for turbulent flows. Flow and heat transfer measurements showed that stabilising effects of favourable pressure gradients caused thinner boundary layers, fuller velocity profiles and corresponding higher heat transfer rates. Downstream laminar and turbulent heat transfer measurements were below the flat plate laminar analytical solution and turbulent correlation by 54.2/100 and 25/100 respectively.
机译:在低速风洞中对凸表面边界层进行了实验研究,其中层流压力梯度(k)为-3.6×10〜-6≤k≤+≤3.6×10〜-6,-3.6×10〜湍流为-6≤k≤+ 3.6×10〜-6。流动和传热测量结果表明,有利的压力梯度的稳定作用会导致边界层变薄,速度分布更充分和相应的传热速率更高。下游层流和湍流传热测量值低于平板层流分析溶液,湍流相关性分别低于54.2 / 100和25/100。

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