Flutter based aeroelastic optimization of an aircraft wing with analytical approach

Keyphrases

• Aircraft Wing 100%
• Analytical Approach 100%
• Aeroelastic Optimization 100%
• Flutter 100%
• AGARD 445.6 Wing 83%
• Wing Model 66%
• Elastic Modulus 33%
• Span-wise 33%
• Uncertainty Quantification 33%
• Flutter Analysis 33%
• Shear Modulus 33%
• Flutter Boundary 33%
• Optimization Study 16%
• Three-dimensional (3D) 16%
• Benchmark Problems 16%
• Coefficient of Variation 16%
• Prediction Method 16%
• Structural Effect 16%
• Taper Ratio 16%
• Aerodynamic Loads 16%
• Monte Carlo Simulation Method 16%
• Sweep Angle 16%
• Theodorsen Function 16%
• Optimum Configuration 16%
• Load Calculation 16%
• Model Configuration 16%
• Material Uncertainty 16%
• Random Parameters 16%
• Lagrange Formulation 16%
• Assumed Modes 16%
• Structural Randomness 16%
• Aeroelastic Modeling 16%
• Flutter Prediction 16%
• Boundary Uncertainty 16%
• Modeling Function 16%

Engineering

• Wings 100%
• Analytical Approach 100%
• Uncertainty Quantification 100%
• Benchmark Problem 50%
• Coefficient of Variation 50%
• Reference Data 50%
• Simulation Method 50%
• Aerodynamic Load 50%
• Input Parameter 50%
• Lagrange 50%
• Shear Modulus 50%
• Theodorsen 50%
• Sweep Angle 50%
• Load Calculation 50%
• Modulus of Shear 50%
• Structural Effect 50%
• Modulus of Elasticity 50%