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The heat/mass transfer analogy for a simulated turbine blade
S. Han, Richard J Goldstein
Mechanical Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
19
Scopus citations
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Keyphrases
Turbine Blade
100%
Heat Mass Transfer
100%
Heat Transfer
66%
Mass Transfer Measurements
66%
Gas Turbine
33%
Nusselt number
33%
Sherwood number
33%
Heat Transfer Coefficient
33%
Geometric Conditions
33%
Turbine Cascade
33%
Mass Transfer Experiment
33%
Temperature Boundary Condition
33%
Heat Transfer Experiment
33%
Engineering
Blade Turbine
100%
Boundary Condition
100%
Gas Turbine
50%
Constant Temperature
50%
Nusselt Number
50%
Sherwood Number
50%
Heat Transfer Coefficient
50%
Heat Transfer
50%
Chemical Engineering
Heat Transfer
100%
Heat Transfer Coefficient
100%
Nusselt Number
100%