Assessment of NO_x emissions of the Scimitar engine at Mach 5 based on a thermodynamic cycle analysis

Keyphrases

• NOx Emission 100%
• Scimitar Engine 100%
• Thermodynamic Cycle Analysis 100%
• Cruising Speed 66%
• Air Flow Rate 66%
• Fuel Flow Rate 66%
• Cruise Altitude 66%
• Hybrid System 33%
• Combustion 33%
• NO Emission 33%
• Combustion Chamber 33%
• Propulsion System 33%
• Helium 33%
• Thermodynamic Model 33%
• Transfer Heat 33%
• Formation Reaction 33%
• Nonlinear System of Equations 33%
• Ramjet 33%
• Advanced Propulsion 33%
• Turbofan 33%
• Inverse Effect 33%
• NO2 Emissions 33%
• Equilibrium Model 33%
• Dissociation Reaction 33%

Engineering

• Airflow Rate 100%
• Fuel Flow 100%
• Cycle Analysis 100%
• Flow Rate 50%
• Nonlinear System 50%
• Equilibrium Model 50%
• Combustion Chamber 50%
• Propulsion System 50%
• Thermodynamic Model 50%