DONG Ming. Direct numerical simulation of a spatially evolving hypersonic blunt cone turbulent boundary layer at Mach 6[J]. ACTA AERODYNAMICA SINICA, 2009, 27(2): 199-205.
Citation: DONG Ming. Direct numerical simulation of a spatially evolving hypersonic blunt cone turbulent boundary layer at Mach 6[J]. ACTA AERODYNAMICA SINICA, 2009, 27(2): 199-205.
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Direct numerical simulation of a spatially evolving hypersonic blunt cone turbulent boundary layer at Mach 6

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