Computation of flow and heat transfer of a blade internal cooling passage with truncated v-shaped ribs on opposite walls

Engineering

• Opposite Wall 100%
• Melting Point 33%
• Reynolds' Number 33%
• Fluid Flow 33%
• Thermal Performance 33%
• Gas Turbine 33%
• Side Wall 33%
• Power Output 33%
• Pressure Loss 33%
• Turbulent Flow 33%
• Inlet Temperature 33%
• Thermodynamic Efficiency 33%
• Gas Turbine Engine 33%
• Midsection 33%