A Detailed Analysis of Film Cooling Physics: Part III— Streamwise Injection With Shaped Holes
By D. Hyams, J. Leylek. 2000
161 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering
View Paper: https://www.semanticscholar.org/paper/285ca9de1a4f943d22cf9fe53b6c1d7d1e6dc8f5
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In Aerospace Engineering
In Computational Mechanics
In Mechanical Engineering
Citations in the corpus
- ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, unknown): “Geometries included conical, laidback, and fanshaped holes [2-6], and many novel designs: bean-shaped [7], cusp-shaped [8], crescent-shaped [9], cratered [10], “Console” [11], double-jet [12], Nekomimi [13], transonic wall jet [14], waist-shaped [15], arrowhead-shaped [16], and anti-vortex holes [17”
- Film cooling effectiveness: Comparison of adiabatic and conjugate heat transfer CFD models (2009, background): “Leylek [7] examined the film cooling process for a shaped, streamwise injected, inclined jet for a blowing ratio of 1.”
- Shape optimization of a fan-shaped hole to enhance film-cooling effectiveness (2010, background): “, Bohn and Moritz [10], Hyams and Leylek [11], Azzi and Jubran [12], Miao and Wu [13], Leedom and Acharya [14], and Mahmood et al.”