Effective Control of Turbine Blade Tip Vortices Using Squealer Tips - GridPro Blog
Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance - ScienceDirect
Numerical investigations on the unsteady leakage flow and heat transfer characteristics of the turbine blade squealer tip
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
EP1057972A2 - Turbine blade tip with offset squealer - Google Patents
COMPRESSOR TURBINE ASSEMBLY (AVIM) - TM-55-2840-251-23_214
ROTOR BLADE-TIP SURFACE MESH HIGHLIGHTING SQUEALER TIP RESOLUTION. | Download Scientific Diagram
Rebuild method of a turbine blade tip squealer - Patent 1650404
Uncertainty quantification of the effects of squealer tip geometry deviation on aerothermal performance - Wei Shi, Pingting Chen, Xueying Li, Ren Jing, Hongde Jiang, 2020
Turbine Rotor with Various Tip Configurations Flow and Heat Transfer Prediction
Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance - ScienceDirect
Effects of flow structure on heat transfer of squealer tip in a turbine rotor blade - ScienceDirect
Effects of the Ribbed-Squealer Tip on the Blade Tip Aerothermal Performance in a High Pressure Gas Turbine Cascade
The flow structure inside the squealer tip clearance. (a) 3D... | Download Scientific Diagram
Effective Control of Turbine Blade Tip Vortices Using Squealer Tips - GridPro Blog
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
Turbine Blade Cooling › CAESES
Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance - ScienceDirect
Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar
Effect of shelf squealer tip configuration on aerothermal performance of gas turbine blade - ScienceDirect
Research on turbine blade squealer tip film holes arrangement and moving shroud | Aerospace Systems
![PDF] Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/8f68a05aeba999dc1022506404ae9a2fbeff2942/3-Figure2-1.png "PDF] Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance | Semantic Scholar")
PDF] Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance | Semantic Scholar
EP1650404A2 - Rebuild method of a turbine blade tip squealer - Google Patents
Investigated tip geometries: (a) single squealer (b) optimized squealer... | Download Scientific Diagram
Turbine computational domain with single squealer tip shape. | Download Scientific Diagram
