Multi-objective optimization design of aerothermal performance for turbine blade squealer tip with inclined suction-side rim
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Reference43 articles.
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2. Effects of flow structure on heat transfer of squealer tip in a turbine rotor blade;Zou;Int. Commun. Heat Mass Tran.,2020
3. Uncertainty quantification and sensitivity analysis of aerothermal performance for the turbine blade squealer tip;Huang;Int. J. Therm. Sci.,2022
4. An experimental investigation of adiabatic film cooling effectiveness and heat transfer coefficient on a transonic squealer tip;Saul;ASME J. Turbomach.,2019
5. Effects of the squealer winglet structures on the heat transfer characteristics and aerodynamic performance of turbine blade tip;Jiang;Int. J. Heat Mass Tran.,2019
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