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The effects of Reynolds number, rotor incidence angle, and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage

The effects of Reynolds number, rotor incidence angle, and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage

By Michael F. Blair

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Publish Date

1989

Publisher

United Technologies Research Center,National Aeronautics and Space Administration

Language

eng

Pages

-