Numerical investigation on film cooling of gas turbine blade using anti-vortex holes
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Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0070811
Reference21 articles.
1. Film Cooling From Shaped Holes
2. The effect of turbulence intensity on film cooling of gas turbine blade from trenched shaped holes
3. J. C. Han and A. Rallabandi, Frontier. Heat Mass Transfer (FHMT), 1(1), 1–10 (2010).
4. Film cooling performance of converging slot-hole rows on a gas turbine blade
5. Influence of shaped injection holes on turbine blade leading edge film cooling
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