Design exploration of aerodynamic wing shape for reusable launch vehicle flyback booster

Engineering

• Flight Condition 100%
• Optimization 66%
• Wings 66%
• Reusable Launch Vehicle 66%
• Visualization 33%
• Cost Reduction 33%
• Objective Function 33%
• Nondominated Solution 33%
• Subsonic Flight 33%
• Pitch Moment 33%
• Aerodynamic Centre 33%
• Zeros 33%
• Design 33%
• Stages 33%
• Maps 33%
• Natural Resources Exploration 33%
• Orbits 33%

Physics

• Aerodynamics 66%
• Reusable Launch Vehicles 66%
• Shapes 66%
• Optimization 66%
• Transonic Flight 66%
• Transonic Flow 33%
• Data Mining 33%
• Supersonic Flight 33%
• Value 33%
• Information 33%
• Exploration 33%
• Drag 33%
• Space Transportation 33%