Design of a small pressure chamber to evaluate probe calibrations at varying Reynolds numbers

Keyphrases

• Aerodynamic Probes 25%
• ANSYS Fluent 25%
• Axial Compressor 50%
• Compressible Gas 25%
• Design Study 25%
• Fast Response 25%
• Five-hole Probe 25%
• Flow Behavior 25%
• Flow Condition 25%
• Flow Density 25%
• Free Stream 25%
• High Reynolds number 25%
• Hot-wire Probe 50%
• Mach number Effect 25%
• Mass Flow 25%
• Measurement Area 25%
• Munich 25%
• Numerical Results 25%
• Numerical Simulation 25%
• Pre-design 25%
• Pressure Chamber 100%
• Probe Calibration 100%
• Propulsion 25%
• RANS Simulation 25%
• Reynolds number 100%
• Technical University 25%
• Turbomachinery 50%
• Validation Process 25%
• Wind Tunnel 50%

Engineering

• Additional Component 25%
• Aerodynamics 25%
• Ansys Fluent 25%
• Axial Compressors 50%
• Chamber Pressure 100%
• Compressible Gas 25%
• Deep Understanding 25%
• Experimental Investigation 25%
• Fast Response 25%
• Flow Behavior 25%
• Flow Condition 25%
• Free Flow 25%
• High Reynolds Number 25%
• Hot-Wire Probe 50%
• Mach Number 25%
• Mass Flow Density 25%
• Numerical Study 25%
• Probe Calibration 100%
• Process Validation 25%
• Reynolds' Number 100%
• Test Rig 25%
• Tunnel 50%
• Turbomachinery 50%