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    Computed Temperature Distribution and Cooling of Solid Gas-Turbine Blades (1947)
    In:  CASI
    Details
    Publication Date: 2019-08-17
    Description: Computations were made to determine the temperature distribution and cooling of solid gas-turbine blades.A range of temperatures was used from 1500 degrees to 2500 degrees F, blade-root temperatures from 100 degrees to 1000 degrees F, blade thermal conductivity from 8 to 220 BTU/(hr)(sq ft)(degrees F/ft), and net gas to metal heat transfer coefficients from 75 to 250 BTU/(hr)(sq ft)(degrees F).
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E7B11h
    Format: application/pdf
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