Effect of coolant temperature and mass flow on film cooling of turbine blades

An edition of Effect of coolant temperature and mass flow on film cooling of turbine blades (1997)

Effect of coolant temperature and mass flow on film cooling of turbine blades

By Vijay Kumar Garg

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1997

Publisher

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

Language

eng

Pages

Description:

subjects: Stagnation temperature, Stagnation pressure, Hole distribution (Mechanics), Rotors, Compressibility, Turbine blades, Film cooling