Low Observable Uncrewed Aerial Vehicle Wind Tunnel Model Design, Manufacturing, and Aerodynamic Characterization

Keyphrases

• Wind Tunnel Test 100%
• Model Design 100%
• Wind Tunnel Model 100%
• Aerodynamic Characterization 100%
• Low Observable 100%
• Uncrewed Aerial Vehicle 100%
• Rapid Prototyping 66%
• OpenFOAM 33%
• Deflection 33%
• Cost Reduction 33%
• Numerical Simulation 33%
• Stiffness 33%
• Effective Method 33%
• Reinforced 33%
• Fast Method 33%
• Numerical Results 33%
• Flow Pattern 33%
• Performance Results 33%
• Aerodynamic Characteristics 33%
• Aerodynamic Performance 33%
• Leading Edge Vortex 33%
• Fused Deposition Modeling 33%
• University of Glasgow 33%
• Machining Process 33%
• Aerodynamic Database 33%
• Laser Cutting 33%
• Prototype Model 33%
• Cheaper Method 33%
• Acquisition Time 33%
• Acquisition Cost 33%
• Metallic Parts 33%
• Low-speed Wind Tunnel 33%
• Computer numerical Control Machining 33%
• Wingtip 33%
• Rapid Prototyping Model 33%
• Database Development 33%
• Metallic Inserts 33%
• Tunnel Facility 33%

Engineering

• Wind Tunnel Test 100%
• Aerodynamic Model 100%
• Observables 100%
• Design Model 100%
• Rapid Prototyping 66%
• Test Campaign 33%
• Computer Numerical Control 33%
• Leading Edge Vortex 33%
• Aerodynamic Performance 33%
• Fused Deposition Modeling 33%
• Aerodynamic Characteristic 33%
• Low Wind Speed 33%
• Acquisition Time 33%
• Aerodynamic Database 33%
• Wingtips 33%
• Computer Simulation 33%
• Flow Distribution 33%