Novel multi-stage vortex cooling with bypass for turbine blade leading edge design considering rotational effect
Author:
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference35 articles.
1. Influence of Biot number and geometric parameters on the overall cooling effectiveness of double wall structure with pins;Liu;Appl. Therm. Eng.,2021
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4. Numerical study on flow and heat transfer characteristics of swirling jet on a dimpled surface with effusion holes at turbine blade leading edge;Kong;Appl. Therm. Eng.,2022
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1. Novel adjustable backflow structure in electric coolant pump for balancing hydraulic performance and reducing temperature rise;Applied Thermal Engineering;2024-07
2. Comparison of Showerhead Film Cooling and Double Wall Cooling in a Guide Vane Leading Edge with Hot Streak;International Journal of Gas Turbine, Propulsion and Power Systems;2024
3. Transient film outflow performances of laminated cooling configurations in leading edges of turbine vane;Applied Thermal Engineering;2023-10
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