Effects of the Ribbed-Squealer Tip on the Blade Tip Aerothermal Performance in a High Pressure Gas Turbine Cascade

Engineering

• Gas Turbine 100%
• Leakage Flow 100%
• Blade Tip 100%
• Aerothermal Performance 100%
• Pressure Gas 100%
• Thermal Load 66%
• Heat Transfer Coefficient 33%
• Vortex 33%
• Reynolds-Averaged Navier-Stokes 33%
• Navier-Stokes Equation 33%
• Axial Direction 33%
• Pressure Difference 33%
• Mass Transport 33%
• Circumferential Direction 33%
• Lateral Pressure 33%