Flow characterization of a supersonic and hypersonic arc-heated wind tunnel

Keyphrases

• Nozzle 100%
• Hypersonic 100%
• Arc-heated Wind Tunnel 100%
• Flow Characterization 100%
• Condensation 40%
• Stagnation Temperature 40%
• Pitot Pressure 40%
• Flow Regions 20%
• Root Mean Square 20%
• Frequency up 20%
• Flow Field 20%
• Combustion 20%
• Mach number 20%
• Nozzle Exit 20%
• Uniform Flow 20%
• Axial Length 20%
• Flow Regime 20%
• Pressure Transducer 20%
• Supersonic Flow 20%
• Stagnation Pressure 20%
• Static Pressure 20%
• Angularity 20%
• Hypersonic Wind Tunnel 20%
• Flow Quality 20%
• Pitot 20%
• Spectral Content 20%
• University of Notre Dame 20%
• Hypersonic Flow 20%
• Pressure Probe 20%

Engineering

• Stagnation Temperature 100%
• Pressure Sensor 100%
• Mach Number 50%
• Nozzle Exit 50%
• Uniform Flow 50%
• Flow Regime 50%
• Flow Region 50%
• Stagnation Pressure 50%
• Supersonic Flow 50%
• Exit Plane 50%
• Static Pressure 50%
• Pressure Probe 50%
• Angularity 50%
• Hypersonic Flows 50%
• Flow Distribution 50%