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Adiabatic wall temperature and heat transfer downstream of injection through two rows of holes
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The article was published on 1977-03-01 and is currently open access. It has received 43 citations till now. The article focuses on the topics: Heat transfer coefficient & Heat flux.read more
Citations
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Journal ArticleDOI
Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: Part I effectiveness
TL;DR: Yuen and Martinez-Botas as mentioned in this paper investigated the effects of adding inline and staggered rows for each streamwise angle and pitch-to-diameter ratio. But they focused on a single cylindrical hole at the same inclinations.
Journal ArticleDOI
Correlation of Film-Cooling Effectiveness From Thermographic Measurements at Enginelike Conditions
TL;DR: In this paper, the effect of single parameters and their interactions on the laterally effective adiabatic film cooling on a flat plate surface downstream of a row of cylindrical holes is investigated.
Journal ArticleDOI
Assessment of Various Film Cooling Configurations Including Shaped and Compound Angle Holes Based on Large Scale Experiments
TL;DR: In this paper, the authors compared four different film cooling hole configurations: a single row of fanshaped holes with and without a compound injection angle, a double row of cylindrical holes and a double-row of discrete slots, both in staggered arrangement.
Journal ArticleDOI
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP
TL;DR: In this article, the effect of density ratio on the film cooling effectiveness is coupled with varying blowing ratio (M = 0.25-2.0), freestream turbulence intensity (Tu = 1% −12.5%), and film hole geometry.
Journal ArticleDOI
Film cooling from two rows of holes with opposite orientation angles: injectant behavior and adiabatic film cooling effectiveness
TL;DR: In this paper, the authors measured boundary layer temperature distributions in the streamwise normal plane to illustrate the interaction between the injectant from the holes in the upstream row and from the downstream row.
References
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Journal ArticleDOI
Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: Part I effectiveness
TL;DR: Yuen and Martinez-Botas as mentioned in this paper investigated the effects of adding inline and staggered rows for each streamwise angle and pitch-to-diameter ratio. But they focused on a single cylindrical hole at the same inclinations.
Journal ArticleDOI
Correlation of Film-Cooling Effectiveness From Thermographic Measurements at Enginelike Conditions
TL;DR: In this paper, the effect of single parameters and their interactions on the laterally effective adiabatic film cooling on a flat plate surface downstream of a row of cylindrical holes is investigated.
Journal ArticleDOI
Assessment of Various Film Cooling Configurations Including Shaped and Compound Angle Holes Based on Large Scale Experiments
TL;DR: In this paper, the authors compared four different film cooling hole configurations: a single row of fanshaped holes with and without a compound injection angle, a double row of cylindrical holes and a double-row of discrete slots, both in staggered arrangement.
Journal ArticleDOI
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP
TL;DR: In this article, the effect of density ratio on the film cooling effectiveness is coupled with varying blowing ratio (M = 0.25-2.0), freestream turbulence intensity (Tu = 1% −12.5%), and film hole geometry.
Journal ArticleDOI
Film cooling from two rows of holes with opposite orientation angles: injectant behavior and adiabatic film cooling effectiveness
TL;DR: In this paper, the authors measured boundary layer temperature distributions in the streamwise normal plane to illustrate the interaction between the injectant from the holes in the upstream row and from the downstream row.
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