Investigation of tip impingement cooling scheme on film cooling and aerothermal performance of turbine blade squealer tips with hollow ribs

Aerospace Science and Technology 2026

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Authors: Zuohong Zhou, Bai Bo, Zhigang Li, Jun Li
DOI: 10.1016/j.ast.2026.111632
Cited by: 3
References: 29

Fields of Study & Subjects

Turbomachinery Performance and Optimization Bladed Disk Vibration Dynamics Heat Transfer Mechanisms

Publication details

Journal / source
Aerospace Science and Technology
Publisher
Elsevier BV
Volume
171
Pages
111632–111632
Publication date
9 January 2026
Language
EN