Heat transfer and pressure drop in blade cooling channels with turbulence promoters

Heat transfer and pressure drop in blade cooling channels with turbulence promoters - - Washington, D.C. National Aeronautics and Space Administration (NASA) 1984 - 153 p. - NASA CR 3837 : 1984 .





Turbine blade, Heat transfer, Augmentation, Turbulent heat transfer

LNASA CR 3837 : 1984

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