Consequence of distance among film cooling hole and vortex generator in the film cooling application of gas turbine blade

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Authors: Nirmal Halder
Cited by: 1
References: 43

Fields of Study & Subjects

Turbomachinery Performance and Optimization Heat Transfer Mechanisms Thermodynamic and Exergetic Analyses of Power and Cooling Systems

Publication details

Journal / source
International Journal of Thermal Sciences
Publisher
Elsevier BV
Volume
230
Pages
111110–111110
Publication date
3 July 2026
Language
EN