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“…Ta-narro等人 [32] 在Bobke等人 [31] 的基础上继续探究了机翼 表面逆压力梯度对湍流边界 层的影响, 观察到逆压力 梯度会缩小湍流拟序结构的尺度. Shalaev等人 [33,34] 总 结了三维边界层理论在过去60年内的研究成果. Lee 和Jiang [35] 归纳了层流边界层转捩和湍流产生机制的 成果.…”
Section: 柱体会出现有规律的交替涡结构 提出了著名的Vonunclassified
“…Ta-narro等人 [32] 在Bobke等人 [31] 的基础上继续探究了机翼 表面逆压力梯度对湍流边界层的影响, 观察到逆压力 梯度会缩小湍流拟序结构的尺度. Shalaev等人 [33,34] 总 结了三维边界层理论在过去60年内的研究成果. Lee 和Jiang [35] 归纳了层流边界层转捩和湍流产生机制的 成果.…”
Section: 柱体会出现有规律的交替涡结构 提出了著名的Vonunclassified
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