Effects of inclined suction-side squealer and film cooling schemes on tip aerothermal characteristics for a turbine blade

Aerospace Science and Technology 2026

View at publisher

Authors: Hequn Li, Han Yan, Songtao Wang, Xun Zhou

DOI: 10.1016/j.ast.2026.111970

Cited by: 2

References: 36

Fields of Study & Subjects

Turbomachinery Performance and Optimization Heat Transfer Mechanisms Bladed Disk Vibration Dynamics

References 36