An experimental examination of cantilevered and shrouded stators in a multistage axial compressor

Keyphrases

• Rotor 100%
• Stator 100%
• Vortex 100%
• Experimental Examination 100%
• Multistage Axial Compressor 100%
• Shrouded Stator 100%
• Cantilevered Stator 100%
• Hub Clearance 100%
• Stall Margin 66%
• Traverse Measurement 66%
• Secondary Flow 33%
• Stabilizing Effect 33%
• Radial Profile 33%
• High Pressure 33%
• Operating Point 33%
• Blade pitch Angle 33%
• Total Pressure 33%
• Reconstruction Analysis 33%
• Peak Efficiency 33%
• Flow Injection Analysis 33%
• Static Pressure 33%
• Free End 33%
• Flow Angle 33%
• Low-pressure Compressor 33%
• Annulus 33%
• Total Flow 33%
• Pressure Angle 33%
• Axial Location 33%
• Multistage Compressor 33%
• Pressure-rise Coefficient 33%
• Controlled Diffusion Airfoil 33%
• Through-flow Code 33%
• Compressor Facilities 33%
• Near Stall Condition 33%

Engineering

• Multistage 100%
• Rotors 100%
• Vortex 100%
• Axial Compressors 100%
• Experimental Investigation 33%
• Operating Point 33%
• Peak Efficiency 33%
• Pressure Rise 33%
• Flow Analysis 33%
• Axial Location 33%
• Exit Plane 33%
• Multistage Compressor 33%
• Airfoil 33%
• Secondary Flow 33%
• Static Pressure 33%