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Showing 1 to 1 of 1 for “"Aerodynamic Loss, Heat Transfer, Mach Number, Reynolds Numbers, Transition, Vane Cascade"”.
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Heat Transfer, Transition, And Aerodynamic Loss In A Linear Vane Cascade At Low Reynolds Numbers In High Speed Flows
… the low pressure turbine experiences low Reynolds number flow, which produces a laminar boundary layer on airfoil surfaces. The integrity of the laminar boundary layer is highly susceptible to flow disturbances resulting from blade wakes and freestream turbulence. This susceptibility often …