Research of performance evaluation methods for multi-stream plate-fin heat exchanger
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Research of performance evaluation methods for multi-stream plate-fin heat exchanger
Research of performance evaluation methods for multi-stream plate-fin heat exchanger
南京航空航天大学学报(英文版)2017年34卷第5期
作者机构:
苏州科技大学
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纸质出版:2017
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li jun. Research of performance evaluation methods for multi-stream plate-fin heat exchanger[J]. 南京航空航天大学学报(英文版), 2017,34(5).
li jun. Research of performance evaluation methods for multi-stream plate-fin heat exchanger[J]. Transactions of Nanjing University of Aeronautics and Astronautics, 2017, 34(5).
li jun. Research of performance evaluation methods for multi-stream plate-fin heat exchanger[J]. 南京航空航天大学学报(英文版), 2017,34(5).DOI:
li jun. Research of performance evaluation methods for multi-stream plate-fin heat exchanger[J]. Transactions of Nanjing University of Aeronautics and Astronautics, 2017, 34(5).DOI:
Research of performance evaluation methods for multi-stream plate-fin heat exchanger
Mathematical model of cross type multi-stream plate-fin heat exchanger was established. Meanwhile mean square error of accumulative heat load was normalized by dimensionless
and the equations of temperature-difference uniformity factor were improved. Evaluation factors above and performance of heat exchanger were compared and analyzed by taking aircraft three-stream condenser as an example. The results demonstrate that the mean square error of accumulative heat load is common result of total heat load and excess heat load between passages. So it can be influenced by passage arrangement
flow inlet parameters as well as flow patterns. Dimensionless parameter of mean square error of accumulative heat load can reflect the influence of passage arrangement to heat exchange performance and will not change dramatically with the variation of flow inlet parameters and flow patterns. Temperature-difference uniformity factor is influenced by passage arrangement and flow patterns. It remains basically unchanged under a certain range of flow inlet parameters.