Research of low boom and low drag supersonic aircraft design

Engineering

• Computational Fluid Dynamics 16%
• Control Parameter 16%
• Design Environment 50%
• Drag Reduction 16%
• Inverse Design Method 16%
• Multiobjective Genetic Algorithm 33%
• Multiobjective Optimization Method 16%
• Non-Dominated Sorting Genetic Algorithm II 16%
• Objective Function 16%
• Pareto Front 16%
• Pareto Solution 16%
• Sonic Boom 50%
• Supersonic Aircraft 100%
• Wave Drag 33%