Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

An edition of Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades (1997)

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

By V. K. Garg

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Publish Date

1997

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Velocity distribution, Coolants, Temperature distribution, Hole geometry (Mechanics), Turbine blades, Film cooling