Development and testing of the ACT-1 experimental facility for hypersonic combustion research

Keyphrases

• Experimental Facility 100%
• Combustion Experiment 100%
• Hypersonic Combustion 100%
• Supersonic Combustor 66%
• Tunnel Facility 66%
• Gas Generator 66%
• Rayleigh Scattering 33%
• Wind Tunnel 33%
• Flight Condition 33%
• Flow Channel 33%
• Optical Diagnostics 33%
• Optical Access 33%
• High Enthalpy 33%
• Combustion Phenomena 33%
• Turbulent Flow Structure 33%
• Flame Structure 33%
• Turbulent Flames 33%
• Laser Diagnostics 33%
• Hypersonic 33%
• Planar Laser 33%
• Stagnation Temperature 33%
• Internal Flow 33%
• Generator System 33%
• Alta 33%
• High-temperature Gas 33%
• Hypersonic Flow 33%
• University of Notre Dame 33%
• Flame Holder 33%
• OH Planar Laser Induced Fluorescence 33%
• Turbulent Combustion 33%
• Wall Cavity 33%
• Hypersonic Wind Tunnel 33%
• Pulsed Arc 33%
• Compression Ramp 33%
• Constant Cross-section 33%
• Fuel Nozzle 33%
• Vacuum Test 33%
• High-speed Flight 33%
• High-speed Schlieren Imaging 33%
• Scramjet Inlet 33%
• Scramjet Combustor 33%
• Open-type 33%

Physics

• Supersonics 100%
• Combustion Chamber 100%
• Hypersonic Combustion 100%
• Wind Tunnels 66%
• Hypersonics 66%
• Supersonic Combustion Ramjet Engine 66%
• Enthalpy 33%
• Rayleigh Scattering 33%
• Turbulent Flow 33%
• Laser Induced Fluorescence 33%
• High Temperature Gas 33%
• Hypersonic Flow 33%
• Turbulent Combustion 33%
• Stagnation Temperature 33%
• Internal Flow 33%
• Flame Holder 33%

Engineering

• Combustor 100%
• Test Rig 100%
• Gas Generator 66%
• Flow Channel 33%
• Flight Condition 33%
• Test Section 33%
• Schlieren 33%
• Turbulent Flow 33%
• Planar Laser-Induced Fluorescence 33%
• Laser Diagnostics 33%
• Stagnation Temperature 33%
• Internal Flow 33%
• Hypersonic Flows 33%
• Jet Nozzle 33%
• Pulsed Arc 33%
• Cross-Section Constant 33%