Multidisciplinary uncertainty quantification in aeroelastic analyses of semi-span supersonic transport wing

Keyphrases

• Aeroelastic Analysis 100%
• Uncertainty Quantification 100%
• Supersonic Transport 100%
• Model Order Reduction 50%
• Quantification Studies 50%
• Computation Time 25%
• Design Parameters 25%
• Monte Carlo Simulation 25%
• Angle of Attack 25%
• Proper Orthogonal Decomposition 25%
• Time Requirement 25%
• Elastic Modulus 25%
• Sampling Methods 25%
• Number of Function Evaluations 25%
• Output Parameters 25%
• Aeroelasticity 25%
• Aerodynamic Model 25%
• Latin Hypercube Sampling 25%
• Reduced Order Model 25%
• Structure Analysis 25%
• Aerodynamic Uncertainty 25%
• Flutter Analysis 25%
• Fidelity Analysis 25%
• Polynomial Chaos Expansion 25%
• Dynamic Pressure 25%
• Static Aeroelastic Analysis 25%
• Multidisciplinary Analysis 25%
• Structural Uncertainty 25%
• Flutter 25%
• Random Parameters 25%
• Cumulative Distribution 25%
• Dynamic Angle 25%
• Static Aeroelastic 25%
• Coupled Fluid-structure Interaction 25%

Engineering

• Uncertainty Quantification 100%
• Model Reduction 50%
• Angle-of-Attack 25%
• Proper Orthogonal Decomposition 25%
• Structural Model 25%
• Function Evaluation 25%
• Output Parameter 25%
• Aerodynamic Model 25%
• Dynamic Pressure 25%
• Latin-Hypercube Sampling 25%
• Reduced Order Model 25%
• Design Parameter 25%
• Sampling Technique 25%
• Computational Time 25%
• Cumulative Distribution 25%