首页> 外文期刊>International Journal of Thermal Sciences >Development of flat-plate thermal and velocity boundary layers under highly turbulent and instable air flows: Reynolds numbers ranging from 8400 to 127 000
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Development of flat-plate thermal and velocity boundary layers under highly turbulent and instable air flows: Reynolds numbers ranging from 8400 to 127 000

机译:在高度湍流和不稳定的气流下发展平板热边界层和速度边界层:雷诺数从8400到127 000

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摘要

Temperature and velocity profiles were measured in a flat-plate boundary layer subjected to free stream turbulence intensities ranging from 1 to 50% and at Reynolds numbers from 8 400 to 127 000. The greatest turbulence intensity values were accompanied by large scales instabilities into the flow. When Tu{sub}∞≈ 1% the temperature and velocity profiles were in agreement with the Blasius solution providing that the real boundary layer thickness was taken into account. For Tu{sub}∞ ≥6% the thermal and velocity boundary layers greatly thickened as well as the displacement and momentum thicknesses. A "wake region" was observed in the profiles and there was an increase of slopes in the near-wall region of the thermal profiles. Moreover turbulent energy was produced in the boundary layer. Some differences were observed between the thermal and velocity boundary layers which can be explained by the unheated starting length which existed at the leading edge oftheplate.
机译:在自由边界湍流强度为1%至50%且雷诺数为8400至127 000的平板边界层中测量温度和速度分布。最大湍流强度值伴随着大规模不稳定性进入流。当Tu {sub}∞≈1%时,温度和速度曲线与Blasius解一致,条件是要考虑实际边界层的厚度。对于Tu {sub}∞≥6%,热边界层和速度边界层以及位移和动量厚度都大大增厚。在轮廓中观察到“唤醒区域”,并且热轮廓的近壁区域中的斜率增加。此外,在边界层中产生了湍流能量。在热边界层和速度边界层之间观察到一些差异,这可以用存在于板前缘的未加热起始长度来解释。

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