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进人涡流尾迹中的飞机强度
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作者 白九龙 曾冬娟 《飞机设计》 2001年第3期142-147,共6页
关键词 涡流尾迹 飞机强度 安全距离 稳定性
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垂直轴风力机尾迹的时空特性 被引量:1
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作者 田甜 孙翀 +1 位作者 竺晓程 杜朝辉 《动力工程学报》 CAS CSCD 北大核心 2023年第3期341-348,371,共9页
基于非定常流场计算结果,对三叶片垂直轴风力机尾迹流场进行数值模拟,并在叶尖速比为2.65工况下对风力机尾迹流场进行频谱分析,然后采用动力模态分解(DMD)方法对垂直轴风力机尾迹流场进行模态分析。结果表明:近尾迹、过渡区尾迹和远场... 基于非定常流场计算结果,对三叶片垂直轴风力机尾迹流场进行数值模拟,并在叶尖速比为2.65工况下对风力机尾迹流场进行频谱分析,然后采用动力模态分解(DMD)方法对垂直轴风力机尾迹流场进行模态分析。结果表明:近尾迹、过渡区尾迹和远场尾迹区具有不同的频率特征;而DMD分解结果提取了对应上述不同特征频率的流动模态,成功捕捉到了下游尾迹流场中不同尺度的流动结构,前5阶主要模态直观显示了尾迹流场中3个不同区域的流动特征结构。 展开更多
关键词 垂直轴风力机 尾迹涡流 频谱分析 动态模态分解
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Flow characteristics at low Reynolds number around two in-line circular cylinders with slits 被引量:1
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作者 SUN Zhi-qiang ZHANG Yu-zhuo +1 位作者 XING Peng-fei LI Sai-wei 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第8期2021-2028,共8页
This study investigated numerically the characteristics of laminar flow around two identical circular cylinders placed in tandem, with slits of the same width through their respective axis. The center to center distan... This study investigated numerically the characteristics of laminar flow around two identical circular cylinders placed in tandem, with slits of the same width through their respective axis. The center to center distance between the cylinders and the slit orientation were varied to study their effects on the flow structure, lift and drag, and vortex shedding characteristics. It was found that three flow regimes could be distinguished, the transitions between which could be indicated by the sudden changes in drag and lift. Asymmetrically, configured slits destabilized the stagnant region between cylinders;whereas in-line slits connect the two cylinders to act as a single elongated bluff body, even at large cylinder separation, by stabilizing the stagnant region in between. These in turn strongly modified the transition between flow regimes. Vortex shedding was also strongly influenced by both slit configuration and cylinder separation. 展开更多
关键词 two cylinders in tandem circular cylinder with slit vortex shedding laminar wake flow
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