Transition prediction and sensitivity analysis for a natural laminar flow wing glove flight experiment

Engineering

• Aerodynamic Drag 16%
• Aerodynamic Efficiency 16%
• Aircraft Aerodynamics 16%
• Angle-of-Attack 16%
• Laminar Flows 100%
• Linearized Stability 33%
• Number Distribution 16%
• Pressure Distribution 33%
• Pressure Gradient 33%
• Relative Error 16%
• Reynolds' Number 50%
• Transport Aircraft 33%