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Figure 1-14.--Blade with squealer tip.
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7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]
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A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020
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Influence of uneven blade tip clearances on aeroacoustic characteristics of centrifugal compressors
A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020
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HFCL]한국항공대학교 열유동제어 연구실
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7.1.1 Fundamentals of Blade Tip Rubbing [Aeroengine Safety]
Aerospace | Free Full-Text | Turbine Blade Tip External Cooling Technologies
WES - CFD-based curved tip shape design for wind turbine blades
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Blade tip constant circumferential angle planes drawn for " partial... | Download Scientific Diagram
Numerical investigation of high pressure turbine blade tip-shaping effects on the aerothermal and dynamic performance | Emerald Insight
