Drag reduction on multi-bump technology based on free-form deformation method for flying wing unmanned aerial vehicle coupled with intake and exhaust system

Engineering

• Unmanned Aerial Vehicle 100%
• Exhaust System 100%
• Drag Reduction 100%
• Intake System 100%
• Freeform Deformation 100%
• Design Optimization 16%
• Genetic Algorithm 16%
• Surrogate Model 16%
• Numerical Model 16%
• Angle-of-Attack 16%
• Aerodynamic Performance 16%
• Skin Friction Drag 16%
• Total Drag 16%
• Attack Angle 16%
• Dimensional Flow Field 16%