A Computational Technique to Evaluate the Relative Influence of Internal and External Cooling on Overall Effectiveness
Document Type
Article
Publication Date
2020
Abstract
Excerpt: Gas turbine components are protected via a coolant that travels through internal passageways before being ejected as external film cooling. Modern computational approaches facilitate the simulation of the conjugate heat transfer that takes place within turbine components, allowing the prediction of the actual metal temperature, nondimensionalized as overall effectiveness.
DOI
10.1115/1.4045987
Source Publication
Journal of Turbomachinery
Recommended Citation
Bryant, C. E., & Rutledge, J. L. (2020). A Computational Technique to Evaluate the Relative Influence of Internal and External Cooling on Overall Effectiveness. Journal of Turbomachinery, 142(5), 142-5_A8_08. https://doi.org/10.1115/1.4045987. Paper # TURBO-19-1123
COinS
Comments
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