Assessment of coolant jet over flat plate surface with two staggered rows of holes by using infrared technology
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AIP Publishing
Reference16 articles.
1. Numerical simulation on film cooling with compound angle of blade leading edge model for gas turbine
2. J. C. Han., S. Dutta, S. V. Ekkad, 2012, “Chapter 3 Turbine Film Cooling,” Gas Turbine Heat Transfer and Cooling Technology, Second Edition, CRC Press-Taylor & Francis Group, Boca Raton, Florida, USA.
3. R. J. Goldstein, “Film Cooling,” Adv. Heat Transf., vol. 7, pp. 321–379, 1971.
4. Film Cooling Effectiveness From Two-Row of Compound Angled Cylindrical Holes Using PSP Technique
5. Large eddy simulation of film cooling with vortex generators between two consecutive cooling rows
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