Influence of engine inlet and exhaust on flying wing UAV and its mechanism analysis

Engineering

• Unmanned Aerial Vehicle 100%
• Flow Distribution 100%
• Aerodynamic Characteristic 100%
• Aerodynamic Design 50%
• Aircraft Engine 50%
• Cross Section 50%
• Computational Fluid Dynamics 50%
• Pressure Distribution 50%
• Boundary Condition 50%
• Integrated System 50%
• Comparative Analysis 50%
• Pressure Flow 50%