Design of an improved turbine rim-seal

Engineering

• Computational Fluid Dynamics 100%
• Flow Rate 100%
• Rotor Disc 100%
• Flow Velocity 100%
• Rotors 50%
• Rotational Reynolds Number 50%
• Swirl Ratio 50%
• Circumferential 50%
• Boundary Layer 50%
• Gas Turbine 50%
• Computational Time 50%
• Computational Cost 50%
• Concentration Ratio 50%
• Hot Gas 50%
• Incompressible Flow 50%
• Rotating Vortex 50%
• Relative Performance 50%
• Engine Design 50%