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July 10, 2000Journal of Fluid Mechanics

Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5

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SGStephen GuariniAmes Research CenterRMRobert MoserThe University of Texas at AustinKSKarim ShariffAmes Research Center

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Guarini et al. (2000) studied this question.

synapsesocial.com/papers/6a81ef79687698565bf20a4ehttps://doi.org/10.1017/s0022112000008466
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