Design and optimization of bump (compression surface) for diverterless supersonic inlet

Engineering

• Design Parameter 100%
• Pressure Recovery 100%
• Supersonic Aircraft 50%
• Pressure Flow 50%
• Square Regression 50%
• Design Condition 50%
• Flow Condition 50%
• Design of Experiments 50%
• Design Space 50%
• Supersonic Flow 50%
• Duct 50%
• Genetic Algorithm 50%
• Baseline Configuration 50%
• Subsonic Flow 50%
• Objective Function 50%
• Flow Characteristics 50%
• Fitness Function 50%
• Computer Simulation 50%
• Jet Aircraft 50%
• Least Squares Method 50%

Physics

• Supersonics 100%
• Supersonic Flow 20%
• Least Squares Method 20%
• Subsonic Flow 20%
• Genetic Algorithm 20%
• Flow Characteristics 20%
• Numerical Simulation 20%
• Design of Experiments 20%