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Flow and Acoustic Fields of Reynolds Number 10e5, Subsonic Jets with Tripped Exit Boundary Layers

机译：雷诺数为10e5的亚音速喷射器，其出口边界层破裂，其流场和声场

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《AIAA/CEAS Aeroacoustics Conference》|2010年|P.1-18|共18页
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作者
C. Bogey; O. Marsden; C. Bailly;
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中图分类气体动力学（可压缩流体力学）;声的传播;
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专利

1. Large-eddy simulation of the flow and acoustic fields of a Reynolds number 10~5 subsonic jet with tripped exit boundary layers [J] . Bogey C., Marsden O., Bailly C. Physics of fluids . 2011,第3期

机译：雷诺数为10〜5的亚音速急流出口边界层跳动的大涡模拟
2. Effects of moderate Reynolds numbers on subsonic round jets with highly disturbed nozzle-exit boundary layers [J] . Bogey C., Marsden O., Bailly C. Physics of fluids . 2012,第10期

机译：中等雷诺数对具有高度扰动的喷嘴出口边界层的亚音速圆形射流的影响
3. Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets [J] . Bogey C., Marsden O. Physics of fluids . 2013,第5期

机译：在最初受到高度干扰的亚音速射流中，确定喷嘴出口边界层厚度及其相应的雷诺数的影响
4. Flow and Acoustic Fields of Reynolds Number 10e5, Subsonic Jets with Tripped Exit Boundary Layers [C] . C. Bogey, O. Marsden, C. Bailly AIAA/CEAS Aeroacoustics Conference . 2010

机译：Reynolds 10e5的流动和声学领域，具有绊倒出口边界层的亚音速喷射器
5. The acoustic far field of a turbulent boundary layer flow calculated from RANS simulations of the flow [D] . Blanc, Jean-Baptiste 2009

机译：通过流动的RANS模拟计算得出的湍流边界层流的声远场
6. Boundary layer control by a fish: Unsteady laminar boundary layers of rainbow trout swimming in turbulent flows [O] . Kazutaka Yanase, Pentti Saarenrinne 2016

机译：鱼的边界层控制：虹鳟在湍流中游荡的不稳定层流边界层
7. Effects of nozzle-exit boundary-layer profile on the initial shear-layer instability, flow field and noise of subsonic jets [O] . Christophe Bogey, Roberto Sabatini 2019

机译：喷嘴 - 出口边界层轮廓对初剪缺陷，流场和亚音速喷射噪声的影响

Flow and Acoustic Fields of Reynolds Number 10e5, Subsonic Jets with Tripped Exit Boundary Layers

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