Coupling evolution and interaction mechanism of multiple leading-edge coolant vortices and boundary layer in turbine cascade

Journal:

Energy

Published:

2026-05-27

DOI:

10.1016/j.energy.2026.141497

Affiliations:

2

Authors:

4

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Institutions	Authors	Share
Beihang University (BUAA), China	2.000000	0.50
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, BUAA, China	2.000000	0.50

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