Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well

Engineering

• Leakage Flow 100%
• Flow Characteristic 66%
• Rotating Speed 66%
• Aerodynamics 33%
• Rotors 33%
• Computational Fluid Dynamics 33%
• Test Rig 33%
• Air Flow 33%
• Pressure Ratio 33%
• Great Influence 33%
• Flow Velocity 33%
• Flow Rate 33%
• Rotational Speed 33%
• Temperature Rise 33%
• Main Flow 33%
• Rotating Disk 33%
• Flow Mechanism 33%
• Axial Compressors 33%
• Radial Displacement 33%
• Rotating Cavity 33%
• Swirl Ratio 33%
• Distance Sensor 33%