Development of a Mach 5 nonequilibrium-flow wind tunnel

Keyphrases

• Fluorescence Imaging 100%
• Wind Tunnel 100%
• Internal Energy 100%
• Non-equilibrium Flow 100%
• Nitrogen Oxides 100%
• Rotational Temperature 100%
• Planar Laser-induced Fluorescence 100%
• Plenum 100%
• Vibrational Temperature 100%
• Energy Modes 100%
• Airflow 50%
• Three-dimensional (3D) 50%
• Laser-induced Fluorescence 50%
• Non-equilibrium 50%
• Steady State 50%
• Nitrogen Flow 50%
• Nanosecond Discharge 50%
• Temperature Distribution 50%
• CO 2 50%
• Blowdown Wind Tunnel 50%
• Schlieren Imaging 50%
• Burst-mode Laser 50%
• Laser-induced Fluorescence Imaging 50%
• Disequilibrium 50%
• Flow Modeling 50%
• Cylinder Model 50%
• Nozzle Throat 50%
• Single Line 50%
• Flow over a Cylinder 50%
• Pulse Repetition Frequency 50%
• Subsonic Flow 50%
• Model Calculation 50%

Engineering

• Nonequilibrium 100%
• Wind Tunnels 100%
• Planar Laser-Induced Fluorescence 66%
• Rotational 66%
• Internal Energy 66%
• Good Agreement 33%
• Nonequilibrium Steady States 33%
• Test Section 33%
• Single Line 33%
• Nanosecond 33%
• Subsonic Flow 33%
• Laser-Induced Fluorescence Imaging 33%
• Blowdown 33%
• Schlieren 33%
• Pulse Repetition Rate 33%
• Temperature Distribution 33%
• Air Flow 33%

Physics

• Laser Induced Fluorescence 100%
• Wind Tunnels 100%
• Nonequilibrium Flow 100%
• Internal Energy 66%
• Subsonic Flow 33%
• Steady State 33%
• Laser Modes 33%
• Pulse Repetition Rate 33%
• Supersonics 33%
• Air Flow 33%
• Temperature Distribution 33%