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机译:大和薄NACA机翼上低雷诺数流的大涡模拟
University of Tokyo, Sagamihara, Kanagawa 229-8510, Japan,Department of Space Transportation Division currently Japan Railway Central;
Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 229-8510, Japan,Institute of Space and Astronautical Science Department of Space Transportation Division. Member AIAA;
Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 229-8510, Japan,Institute of Space and Astronautical Science Department of Space Transportation Division. Senior Member AIAA;
Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 229-8510, Japan,Space and Astronautical Science, Department of Space Transportation Division. Fellow AIAA;
机译:雷诺数为1.6x10(6)时NACA 0015翼型流动的大涡模拟
机译:利用大涡模拟计算NACA0018机翼的非定常流动和空气动力噪声
机译:NACA0021机翼上流动的高阶隐式大涡模拟
机译:雷诺数为256,000的俯仰NACA0012翼型周围动态流场上不同爆破频率下DBD等离子执行器流量控制效果的大涡模拟。
机译:低雷诺数的弧形Naca 65(1)-412翼型的直接数值模拟:流动分离,稳定性和拉格朗日空气动力学
机译:使用PIV技术以低雷诺数在具有基本空腔的厚钝尾缘翼型上进行流动可视化
机译:NACA0025上低雷诺数流的快速大涡模拟
机译:使用非结构化网格对NaCa 4412翼型周围的流动进行初步大涡模拟