Reduced-order model for efficient generation of a subsonic missile's aerodynamic database

Keyphrases

• Aerodynamic Coefficients 66%
• Aerodynamic Database 100%
• Efficient Generation 100%
• Fast Method 33%
• Feasible Set 33%
• Flow Field 33%
• Flowing Solution 33%
• Full Flow 33%
• Governing Equations 33%
• Industrial Relevance 33%
• Interpolative 33%
• Linear Combination 33%
• Missile 100%
• Missile Aerodynamics 100%
• Modeling Parameters 33%
• Operating Conditions 66%
• Optimization Problem 33%
• Parameter Dependence 33%
• Prediction Accuracy 33%
• Prediction Error 33%
• Proper Orthogonal Decomposition 100%
• Reduced Order Model 100%
• Regime Prediction 33%
• Subsonic Flow 33%

Engineering

• Accurate Prediction 33%
• Aerodynamic Coefficient 66%
• Aerodynamic Database 100%
• Boundary Condition 33%
• Computational Fluid Dynamics 66%
• Feasible Set 33%
• Flow Distribution 33%
• Flow Solution 33%
• Linear Combination 33%
• Multiplicity 33%
• Optimisation Problem 33%
• Prediction Error 33%
• Proper Orthogonal Decomposition 100%
• Reduced Order Model 100%
• Subsonic Flow 33%

Physics

• Aerodynamics 100%
• Boundary Condition 25%
• Charge Flow Device 50%
• Computational Fluid Dynamics 50%
• Flow Distribution 25%
• Subsonic Flow 25%