Exploring TBCC engine inlet design for Ma=5

Engineering

• Turbine 100%
• Combined-Cycle Engine 100%
• Flight Trajectory 66%
• Design Point 50%
• Mach Number 33%
• Design Method 33%
• Flow Distribution 33%
• Pressure Recovery Coefficient 33%
• Aerodynamics 16%
• Boundary Layer 16%
• Boundary Condition 16%
• Performance Analysis 16%
• Main Parameter 16%
• Discretization 16%
• Separation Region 16%
• Core Flow 16%
• Flow Coefficient 16%
• High-Altitude Flight 16%
• Equation Turbulence Model 16%
• Layer Interaction 16%
• Corrected Mass Flow 16%
• Shock Interaction 16%

Material Science

• Mach Number 100%
• Aircraft 50%
• Boundary Layer 50%
• Core Flow 50%