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Prediction of heat transfer characteristics for discrete hole film cooling for turbine blade applications
D. K. Tafti, S. Yavuzkurt
Institute for Computational and Data Sciences (ICDS)
Research output
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Contribution to journal
›
Article
›
peer-review
20
Scopus citations
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Dive into the research topics of 'Prediction of heat transfer characteristics for discrete hole film cooling for turbine blade applications'. Together they form a unique fingerprint.
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Keyphrases
Boundary Layer
20%
Cooling Method
20%
Curved Surface
20%
Discrete Hole
100%
Entrainment Fraction
40%
Film Cooling
100%
Good for
20%
Heat Transfer Characteristics
100%
Heat Transfer Coefficient
20%
Injection Model
20%
Injection Parameters
20%
Injection Process
20%
Injection Ratio
20%
Laminar Boundary Layer
20%
Low Injection
20%
Low Reynolds number
20%
Prediction Scheme
40%
Stanton number
20%
Three-dimensional Effect
20%
Turbine Blade
100%
Two Dimensional
100%
Engineering
Blade Turbine
100%
Boundary Layer
20%
Good Agreement
20%
Heat Transfer Coefficient
20%
Injection Model
20%
Injection Process
20%
Laminar Boundary Layer
20%
Stanton Number
20%
Two Dimensional
100%