Investigation of several fundamental combustion problems in rocket-based combined-cycle engines

Engineering

• Combustor 100%
• Combined Cycle 100%
• Combined-Cycle Engine 100%
• Engineering 40%
• Kinetic Model 40%
• Combustion Mode 40%
• Fossil Fuel 40%
• Mach Number 20%
• Multiscale 20%
• Operating Range 20%
• Heat Release 20%
• Shear Property 20%
• Shear Layer 20%
• Reaction Model 20%
• Turbulent Flow 20%
• Subsonic Flow 20%
• Supersonic Flow 20%
• Transonic Flow 20%
• Flight Altitude 20%
• Spatial Distribution 20%
• Fundamental Problem 20%
• Airstream 20%
• Mixing Layer 20%
• Flow Speed 20%