DYNAMIC STALL PREDICTION THROUGH COMBINING PHYSICAL MODELS AND MACHINE LEARNING

Engineering

• Learning System 100%
• Physical Model 100%
• Wind Tunnel Test 66%
• Test Data 66%
• Aerodynamics 33%
• Simulation Result 33%
• Time Domain 33%
• Neural Network Architecture 33%
• Source Data 33%
• Aerodynamic Performance 33%
• Sample Data 33%
• Performance Prediction 33%
• Data Source 33%
• Flight Safety 33%
• Black-Box Model 33%
• Prediction Problem 33%

Physics

• Machine Learning 100%
• Wind Tunnel Test 100%
• Aerodynamics 100%
• Neural Network 50%
• Multisensor Fusion 50%
• Flight Safety 50%
• Standard Model 50%