Effects of casing cooling slot purge on heat transfer in turbine blade tip and casing
Author:
Affiliation:
1. School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, P.R. China
2. Shanghai Engineering Research Center of Space Engine, Shanghai Institute of Space Propulsion, Shanghai, P.R. China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407782.2023.2194688
Reference24 articles.
1. Time resolved measurements of a turbine rotor stationary tip casing pressure and heat transfer field
2. The Effect of Work Processes on the Casing Heat Transfer of a Transonic Turbine
3. Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer
4. Investigations at the Over-Tip Casing of a High Pressure Turbine Including Off-Design Conditions and Heat Transfer Correlations
5. Numerical investigations of the 3D transonic field and heat transfer at the over-tip casing in a HP-turbine stage
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1. Aerothermal characteristics evaluation for different tip configurations without and with film cooling on transonic turbine;International Communications in Heat and Mass Transfer;2024-04
2. Unsteady numerical study of film cooling and heat transfer on turbine blade squealer tip with coolant jet;Numerical Heat Transfer, Part A: Applications;2024-01
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