Robust aeroelastic design optimization of wing/store configurations based on flutter criteria

Keyphrases

• Design Optimization 100%
• Flutter 100%
• Aeroelastic Design 100%
• Monte Carlo Simulation 50%
• Flutter Analysis 50%
• AGARD 445.6 Wing 50%
• Computation Time 25%
• Optimization Study 25%
• Three-dimensional (3D) 25%
• Material Properties 25%
• Benchmark Problems 25%
• Aeroelasticity 25%
• Wing Design 25%
• Aerodynamics 25%
• Taper Ratio 25%
• Optimization Strategy 25%
• Aerodynamic Loads 25%
• Energy Terms 25%
• Optimization Software 25%
• Deterministic Optimization 25%
• Polynomial Degree 25%
• Sweep Angle 25%
• Theodorsen Function 25%
• Flutter Speed 25%
• Polynomial Chaos Expansion 25%
• Structural Displacement 25%
• Aeroelastic Optimization 25%
• Wing Model 25%
• Structural Uncertainty 25%
• Assumed Modes 25%
• Aeroelastic Modeling 25%
• 2nd Order 25%
• Location Design 25%
• Lagrange Equation 25%
• Store Location 25%
• Robustness Criterion 25%
• Elastic Axis 25%

Engineering

• Design Optimization 100%
• Benchmark Problem 33%
• Reference Data 33%
• Aerodynamic Load 33%
• Energy Term 33%
• Lagrange Equation 33%
• Polynomial Order 33%
• Theodorsen 33%
• Sweep Angle 33%
• Flutter Speed 33%
• Deterministic Design 33%
• Structural Uncertainty 33%
• Computational Time 33%
• Optimization Strategy 33%