Endwall and leading-edge film cooling of turbine blades in a hydrogen-fueled rotating detonation combustor–turbine coupled system

Journal:
Energy
Published:
DOI:
10.1016/j.energy.2025.138307
Affiliations:
3
Authors:
6
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Institutions Authors Share
Ningbo Institute of Industrial Technology (CNITECH), CAS, China
2.500000
 0.42
Jiangsu University (JSU), China
2.000000
 0.33
University of Chinese Academy of Sciences (UCAS), China
1.500000
 0.25
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