Combining multi-objective optimization and numerical simulation
the effects of the key structural parameters of a spiral wound heat exchanger on its flow and heat transfer characteristics were studied. And the simulation groups generated by central composite design were calculated. Simulation results show that the shell-side pressure drop of the spiral wound heat exchanger decreases with the increase of the layer pitch
spiral angle and tube pitch; the shell-side heat transfer coefficient of the spiral heat exchanger decreases with the increase of the layer pitch and increases with the external diameter of the tube
however the coefficient increases firstly with the spiral angle then decreases. The sensitivity analysis also shows that the shell-side flow and heat transfer characteristics are most affected by the spiral angle. Under the working conditions
both pressure drop and heat transfer coefficient are negatively correlated with the layer pitch
and the spiral angle is negatively correlated with the pressure drop but positively correlated with the heat transfer coefficient. Three sets of optimal results were obtained by employing multi-objective genetic algorithm to minimize the shell-side pressure drop and maximize the heat transfer coefficient on successive response surfaces. Compared with the original group
the average heat transfer coefficient is increased by 2.93% while the average pressure drop is reduced by 40.27%
which is of great significance for the study of spiral wound heat exchanger.
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references
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