Dual-pump coherent anti-stokes raman spectroscopy measurements in a dual-mode scramjet

Engineering

• Combustor 100%
• Rotational 50%
• Reynolds-Averaged Navier-Stokes 50%
• Mole Fraction 50%
• Computational Fluid Dynamic Modeling 50%
• Contour Plot 50%
• Large Eddy Simulation 50%
• Test Facility 50%
• Stagnation Temperature 50%

Physics

• Raman Spectroscopy 100%
• Supersonic Combustion Ramjet Engine 100%
• Injector 60%
• Combustion Chamber 40%
• Contours 20%
• Computational Fluid Dynamics 20%
• Large Eddy Simulation 20%
• Stagnation Temperature 20%

Keyphrases

• Scramjet Combustor 50%
• H2 Fuel 25%
• Ramjet 25%
• Resistance Heater 25%