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Propulsive performance of complex flapping foils

By 曹永辉, 朝黎明, 丁浩 and 赵红印

Abstract

以NACA0006翼型为基准翼型,将其前缘部分更换为相对最大厚度较大的NACA0008、NACA0010、NACA0015和NACA0020翼型前缘部分,组成混合翼型。通过流体仿真软件Fluent14.5对基准翼型及混合翼型进行数值模拟计算,并分析扑翼运动的推进性能。结果表明:混合翼型相较于基准翼型对扑翼运动推力系数和推进效率有显著提高

Topics: 扑翼, 混合翼型, 推进性能
Year: 2016
OAI identifier: oai:ir.sia.cn/:173321/19228
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