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Film cooling on a gas turbine blade near the end wall
Richard J Goldstein
, H. P. Chen
Mechanical Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
63
Scopus citations
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Dive into the research topics of 'Film cooling on a gas turbine blade near the end wall'. Together they form a unique fingerprint.
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Keyphrases
Endwall
100%
Film Cooling
100%
Gas Turbine Blade
100%
Passage Vortex
60%
Mass Transfer
20%
Flow Visualization
20%
Transfer Techniques
20%
Pressure Surface
20%
Trailing Edge
20%
Horseshoe Vortex
20%
Chord Length
20%
Coolant Flow
20%
Convex Surface
20%
Local Film
20%
Non-protected Areas
20%
Vortex System
20%
Cooling Jet
20%
Engineering
Gas Turbine
100%
Vortex
100%
Flow Visualization
33%
Chord Length
33%
Coolant Flow
33%
Cooling Performance
33%
Pressure Surface
33%
Convex Surface
33%
Vortex System
33%
Trailing Edge
33%
Horseshoe Vortex
33%
Jet
33%