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Parametric study of rotor tip squealer geometry on the aerodynamic performance of a high subsonic axial compressor stage | Journal of the Brazilian Society of Mechanical Sciences and Engineering
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Energies | Free Full-Text | Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
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Experimental investigation of effects of suction side squealer tip on the aeroelastic stability of a linear oscillating compressor cascade - Hongwei Ma, Chao Jin, Wei Wei, 2017
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Numerical investigations on the unsteady leakage flow and heat transfer characteristics of the turbine blade squealer tip
![Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/704371a277bfb2d9f9f68de67e4eba7e07869054/6-Figure2-1.png)
Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar
![Parametric study of rotor tip squealer geometry on the aerodynamic performance of a high subsonic axial compressor stage | Journal of the Brazilian Society of Mechanical Sciences and Engineering Parametric study of rotor tip squealer geometry on the aerodynamic performance of a high subsonic axial compressor stage | Journal of the Brazilian Society of Mechanical Sciences and Engineering](https://media.springernature.com/m685/springer-static/image/art%3A10.1007%2Fs40430-021-02950-5/MediaObjects/40430_2021_2950_Fig1_HTML.jpg)
Parametric study of rotor tip squealer geometry on the aerodynamic performance of a high subsonic axial compressor stage | Journal of the Brazilian Society of Mechanical Sciences and Engineering
Effects of the Ribbed-Squealer Tip on the Blade Tip Aerothermal Performance in a High Pressure Gas Turbine Cascade
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PDF] Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance | Semantic Scholar
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Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance - ScienceDirect
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Effect of shelf squealer tip configuration on aerothermal performance of gas turbine blade - ScienceDirect
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