Model deformation measurements at ARA

Engineering

• Research Aircraft 100%
• Deformation Model 100%
• Design Condition 100%
• Aircraft Structure 50%
• Computational Fluid Dynamics 50%
• Flow Regime 50%
• Primary Goal 50%
• Pressure Profile 50%
• Unsteady Flow 50%
• Finite Element Method 50%
• Fluid-Structure Interaction 50%
• Lightweight Material 50%

Physics

• Wind Tunnels 100%
• Research Aircraft 100%
• Charge Flow Device 33%
• Computational Fluid Dynamics 33%
• Transonic Flow 33%
• Flow Distribution 33%
• Unsteady Flow 33%
• Aircraft Structure 33%

Material Science

• Aircraft 100%
• Computational Fluid Dynamics 25%
• Fluid-Structure Interaction 25%
• Unsteady Flow 25%