Statistical evaluation on cooling unsteadiness level for a cylindrical film-hole influenced by partial blockage under pulsed mainstream
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference40 articles.
1. Multi-objective optimization on internal cooling strategies for gas turbine blade leading edges;Chen;Int. Commun. Heat Mass Transf.,2023
2. Effects of dislocations on film cooling effectiveness of a laidback fan-shaped hole;Jiang;Int. Commun. Heat Mass Transf.,2023
3. Detailed showerhead cooling effectiveness measurements on the notched leading-edge surface: effect of freestream turbulence and density ratio;Ye;Int. Commun. Heat Mass Transf.,2022
4. Transient film outflow performances of laminated cooling configurations in leading edges of turbine vane;Song;Appl. Therm. Eng.,2023
5. LES of jet-crossflow interactions: flow structures and heat transfer characteristics;Babu,2015
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