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机译:带有尾流的平板边界层的统计和结构的进一步研究
Department of Mechanical Engineering, Royal Military College of Canada, PO Box 17000, Station Forces, Kingston, Ontario, Canada K7K 7B4;
rnDepartment of Mechanical Engineering, Royal Military College of Canada, PO Box 17000, Station Forces, Kingston, Ontario, Canada K7K 7B4;
rnDepartment of Mechanical Engineering, Royal Military College of Canada, PO Box 17000, Station Forces, Kingston, Ontario, Canada K7K 7B4;
rnDepartment of Mechanical Engineering, Royal Military College of Canada, PO Box 17000, Station Forces, Kingston, Ontario, Canada K7K 7B4;
wake perturbation; zero-pressure gradient flat-plate boundary layer; direct numerical simulation; turbulent spot arrowhead; transition mechanisms; three-dimensional visualizations;
机译:有利和不利压力梯度下平板边界层的尾流旁通跃迁实验研究
机译:良好压力梯度对平板超声波湍流边界层湍流结构及误差的影响
机译:周期性尾流通道在平板边界层上经历有利和不利压力梯度的影响
机译:平板边界层的尾波诱导旁路转换研究:小球形尾波和细线尾波引起的两种转换模式的比较
机译:波浪和自由表面对冲孔平板湍流边界层和尾流的影响。
机译:渐近几何结构对湍流边界层动量传输运动的统计证明
机译:周期性唤醒通过平板边界层经历良好且不利的压力梯度的影响
机译:边界层和尾迹中相干结构的Les研究。第二卷:在方形圆筒周围醒来