Multi-jet impingement cooling in the leading edge of turbine blade using matrix as internal structure-Reference-Cited by-同舟云学术

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Multi-jet impingement cooling in the leading edge of turbine blade using matrix as internal structure

Published:2024-08 Issue: Volume:250 Page:123531
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Li Jie,Yu Binye,Li Xingwei,Bu Shi,Wang Ao

Publisher

Elsevier BV

Reference35 articles.

1. Gas turbine heat transfer and cooling technology[M];Han;CRC Press,2012

2. Numerical study of a fully confined supersonic slot impinging jet from bleed system;Huang;Aerosp. Sci. Technol.,2019

3. Flow visualization of a round jet impinging on cylindrical surfaces;Cornaro;Exp. Therm Fluid Sci.,1999

4. Heat/mass transfer measurement on concave surface in rotating jet impingement;Hong;J. Mech. Sci. Technol.,2008

5. Rapid design approach for U-bend of a turbine serpentine cooling passage;Kim;Aerosp. Sci. Technol.,2019

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1. Heat transfer characteristic and optimization design of alter diameter array impingement cooling structure;Applied Thermal Engineering;2024-09

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