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Effect of in-hole roughness on film cooling from a shaped hole
Robert P. Schroeder
, Karen A. Thole
Mechanical Engineering
Research output
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Contribution to journal
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Article
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peer-review
61
Scopus citations
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Dive into the research topics of 'Effect of in-hole roughness on film cooling from a shaped hole'. Together they form a unique fingerprint.
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Keyphrases
Adiabatic Effectiveness
50%
Blowing Ratio
50%
Coolant
25%
Cooling Hole
25%
Core Flow
25%
Effectiveness Evaluation
25%
Film Cooling
100%
Flow Field
25%
Gas Turbine Components
25%
High Blowing Ratio
25%
Interior Walls
25%
Large Roughness
50%
Shaped Holes
100%
Surface Roughness
25%
Thermal Field
25%
Turbulence Intensity
25%
Engineering
Cooling Hole
100%
Core Flow
100%
Gas Turbine
100%
Thermal Field
100%
Turbine Components
100%
Turbulence Intensity
100%