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Development of new correlations for heat transfer and friction loss of solid ring with combined square wing twisted tape inserts heat exchanger tube

机译:结合方形翼形扭曲带状插入式换热器管的固体环的传热和摩擦损失的新关联的开发

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摘要

An experimental analysis has been carried out for heat transfer and turbulent flow in a heat exchanger circular tube with solid ring with combined square wing twisted tape (TT) inserts. Experimentations are performed varying the solid ring with combined square wing TT insert parameters, such as changing the number of TT inserts from 1.0 to 4.0, ring pitch ratio from 0.5 to 2.0, wing pitch ratio from 2.0 to 3.5, wing depth ratio from 0.083 to 0.333, ring diameter ratio from 0.831 to 0.932, and Reynolds number in the range of 3,000-21,000. The experimental results show that the heat transfer is increased around 5.66 times more than the plane circular tube. The thermal hydrodynamic performance is evaluated for the optimum range of solid ring with combined square wing TT insert parameters. Statistical correlations are developed and a deviation of correlation data from the experimental data of Nusselt number and friction factor is about +/- 9% and +/- 6%, respectively. The correlation is helpful in prediction of the thermal performance for turbulent flow through a circular tube with solid ring with combined square wing twisted tape inserts.
机译:已对带有实心环的热交换器圆管中的传热和湍流进行了实验分析,实心环带有组合的方翼扭曲带(TT)插入件。通过组合方翼TT插入件参数来更改实心环,例如将TT插入件的数量从1.0更改为4.0,环节距比从0.5更改为2.0,机翼节距比从2.0更改为3.5,机翼深度比从0.083更改为0.333,环直径比从0.831到0.932,雷诺数在3,000-21,000之间。实验结果表明,传热比平面圆管提高了约5.66倍。通过组合方翼TT插入参数,评估了实心环的最佳范围的热流体动力学性能。统计相关性得到发展,相关性数据与努塞尔数和摩擦系数的实验数据的偏差分别约为+/- 9%和+/- 6%。该关系式有助于预测湍流通过带有实心环并结合有方翼扭曲带状插入件的圆形管的湍流的热性能。

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