Direct numerical simulations of high-speed boundary layer transition including adverse pressure gradients

【Author】

Kenneth Franko;Sanjiva K.Lele;

【Abstract】

<正>Direct numerical simulations of high-speed flat plate boundary layer transition at edge Mach number of 6,for zero pressure gradient and adverse pressure gradients,were undertaken using different disturbance forcing.The simulations used high-order staggered compact scheme with localized artificial dissipation for

【Keywords】

high;mode;Direct numerical simulations of high-speed boundary layer transition including adverse pressure gradients;

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