Influence of converging conical hole angles on jet impingement blade cooling of gas turbine blade leading edge
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Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0070816
Reference19 articles.
1. Evaluation of internal heat-transfer coefficients for impingement-cooled turbine airfoils.
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4. Technical Note The effect of concave surface curvature on heat transfer from a fully developed round impinging jet
5. C. N. Jordan, L. M. Wright, D. C. Crites, Impingement Heat Transfer on a Cylindrical, Concave Surface with Varying Jet Geometries, 2012, ASME Paper No. GT2012-68818.
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