Numerical investigation of the partition rib design and loss reduction mechanism in squealer blade tip

Aerospace Science and Technology 2026

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Authors: Yun Jin, Hongmei Li, Shaopeng Lu, Yushi Bai, Jinfang Teng

DOI: 10.1016/j.ast.2026.111730

Cited by: 5

References: 21

Fields of Study & Subjects

Turbomachinery Performance and Optimization Heat Transfer Mechanisms Combustion and flame dynamics

References 21