Scramjet Intake Design Based on Exit Flow Profile via Global Optimization and Deep Learning toward Inverse Design

Physics

• Supersonic Combustion Ramjet Engines 100%
• Mixing 100%
• Combustion 66%
• Fuel 66%
• Shock Wave 66%
• Computational Fluid Dynamics 66%
• Deep Learning 66%
• Optimization 33%
• Utilization 33%
• Technology 33%
• Ignition 33%
• Geometry 33%
• Engine 33%
• Genetic Algorithm 33%
• Propulsion 33%
• Hypersonic Flight 33%

Computer Science

• Design 100%
• Global Optimization 66%
• Optimization 33%
• Technical Challenge 33%
• Genetic Algorithm 33%
• Computational Cost 33%
• Compression Ratio 33%
• Process Optimization 33%
• Deep Learning Technique 33%
• Quadratic Programming 33%
• Design Exploration 33%

Engineering

• Initial Point 33%