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Numerical and Experimental Studies on the Propulsion Performance of A Wave Glide Propulsor 被引量:8
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作者 刘鹏 苏玉民 廖煜雷 《China Ocean Engineering》 SCIE EI CSCD 2016年第3期393-406,共14页
This paper introduces a newly developed Unmanned Wave Glide Vehicle (UWGV), which is driven only by extracting energy from gravity waves, and presents a comprehensive study on the propulsion performance of the UWGV... This paper introduces a newly developed Unmanned Wave Glide Vehicle (UWGV), which is driven only by extracting energy from gravity waves, and presents a comprehensive study on the propulsion performance of the UWGV's propulsor-Wave Glide Propulsor (WGP) in a regular wave. By simplifying the WGP as six 2D tandem asynchronous flapping foils (TAFFs), a CFD method based on Navier-Stokes equations was first used to analyze the hydrodynamic performance of TAFFs with different parameters of non-dimensional wave length rn and non-dimensional wave height n. Then, a series of hydrodynamic experiments were performed. The computational results agree well with the experimental results when n〈0.07 and both of them show the thrust force and input power of the WGP are larger at smaller m or larger n. By analyzing the flow field of TAFFs, we can see that a larger m is beneficial to the forming, merging and shredding of the TAFFs' vortices; as TAFFs are arranged in tandem and have the same motions, the leading edge vortex and wake vortex of the TAFFs are meaningful for improving the thrust force of their adjacent ones. 展开更多
关键词 Wave Glide Propulsor (WGP) tandem asynchronous flapping foil (taff CFD hydrodynamic experiments propulsion performance
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串列异步拍动翼推进性能分析 被引量:12
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作者 刘鹏 苏玉民 +1 位作者 刘焕兴 廖煜雷 《上海交通大学学报》 EI CAS CSCD 北大核心 2014年第4期457-463,共7页
以滑波推进器为原型,基于RANS方程,采用动网格技术计算了6翼异步拍动翼串列时的水动力性能,探讨了来流、摆幅角、翼间距、运动周期和升沉幅度等对其推进性能的影响,并建造样机.计算结果表明,串列异步拍动翼不同位置翼表现出不同的性能,... 以滑波推进器为原型,基于RANS方程,采用动网格技术计算了6翼异步拍动翼串列时的水动力性能,探讨了来流、摆幅角、翼间距、运动周期和升沉幅度等对其推进性能的影响,并建造样机.计算结果表明,串列异步拍动翼不同位置翼表现出不同的性能,且任一位置翼比单片异步拍动翼产生更大的推力.尾涡分析表明,翼间涡系干扰是不同位置翼性能不同的主要原因,且其干扰对推力的产生有利,小间距时可产生更大推力. 展开更多
关键词 串列异步拍动翼 推进性能 尾涡干扰 动网格
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