College of Energy and Power Engineering Nanjing University of Aeronautics and Astronautics,Nanjing 2I0016,China;
College of Energy and Power Engineering Nanjing University of Aeronautics and Astronautics,Nanjing 210016, China;
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;
College of Aerospace Engineering Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;
large eddy simulation; the horseshoe-shaped vortex; turbulent boundary layer; coherent structures; preconditioned algorithm;
机译:基于断层粒子图像速度测速法的湍流边界层近壁区域主导涡流结构的实验研究
机译:湍流边界层中惯性粒子的近壁堆积区域特征
机译:剪切层结构在湍流边界层近壁区域的传播
机译:湍流边界层近壁区域马蹄形涡流的开发与分析
机译:三维湍流边界层的近壁研究。
机译:PNAS Plus:边界层中的过渡湍流点和湍流湍流点
机译:流动涡旋行对湍流边界层的影响:第1报告,湍流边界层的流动涡旋行的特性和湍流边界层的平均速度场