吴浩, 杨子烨. 大尺度自航模气层减阻试验研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03360
引用本文: 吴浩, 杨子烨. 大尺度自航模气层减阻试验研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03360
Experimental research of air layer drag reduction on large-scale model[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03360
Citation: Experimental research of air layer drag reduction on large-scale model[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03360

大尺度自航模气层减阻试验研究

Experimental research of air layer drag reduction on large-scale model

  • 摘要: 【目的】研究气流量、航行倾角对船底凹槽内气层保持效果和节能效果的影响。【方法】通过设计气层减阻自航模的控制系统和喷气装置,来开展开阔水域条件下自航模气层减阻试验。【结果】在主机转速一定时,喷气可以明显提高自航模的航速,停止喷气后,船底凹槽内的气体能维持较长时间;船体保持正浮状态并且尾倾小于0.25°时的气层减阻效果较好,较大尾倾角时气体从自航模首部两侧溢出,气层无法对船底实现有效覆盖,减阻效果不明显。【结论】通过试验,获得了一些有意义的结论,可对气层减阻技术在肥大型船舶上的工程应用提供一定参考。

     

    Abstract: Objectives The effects of air flow rate, sailing angle within the groove bottom of the air layer retention and energy efficiency were studied. Methods The air injection device and control systems were designed for the experiment of air layer drag reduction on self-propelled model in open waters. Results When the host speed is in certain, it can significantly improve the model speed with air injection, and after stopping the jet the air layer within the air cavity of ship bottom can be maintained for a long time; it will get better drag reduction efficiency when the ship in the upright state and the trimming is within 0.25 degrees. When the trimming angle is too larger, the gas will overflows from both sides of the model head, and the air layer cannot effectively cover the bottom of the ship, so it will decrease the efficiency of the drag reduction. Conclusions Through experiments, some meaningful conclusions have been obtained, which can provide a certain reference for the engineering application of air layer drag reduction technology on large ships.

     

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