Multidisciplinary optimization and design variable sensitivity of helicopter rotor blades using a composite box beam model

Keyphrases

• Multidisciplinary Design 100%
• Beam Model 100%
• Multidisciplinary Design Optimization 100%
• Composite Box Beam 100%
• Variable Sensitivity 100%
• Helicopter Rotor Blade 100%
• Design Requirements 66%
• Structural Design 66%
• Aerodynamic Design 66%
• Dynamic Aerodynamics 66%
• Shear Force 33%
• Multiple Design 33%
• Fully Integrated 33%
• Design Objectives 33%
• Optimization Problem 33%
• Dynamic Structure 33%
• Analysis Procedure 33%
• Two-objective 33%
• Integrated Optimization 33%
• Dynamic Design 33%
• Substantial Reduction 33%
• Programming Techniques 33%
• Load Carrying 33%
• Optimization Procedure 33%
• Critical Dynamics 33%
• Aeroelasticity 33%
• Optimum Design 33%
• Function Approach 33%
• Approximate Analysis 33%
• Kreisselmeier-Steinhauser Function 33%
• Blade Design 33%
• Nonlinear Programming 33%
• Aeroelastic Design 33%
• Blade Aerodynamics 33%
• Blade Dynamics 33%
• Blade Root 33%
• Isotropic Beam 33%
• Beam Element 33%
• Blade Structure 33%

Engineering

• Design Requirement 100%
• Structural Design 100%
• Rotor Blade 100%
• Beam Model 100%
• Helicopter Rotors 100%
• Aerodynamic Design 100%
• Design Objective 50%
• Optimisation Problem 50%
• Objective Function 50%
• Shear Force 50%
• Optimisation Procedure 50%
• Aeroelasticity 50%
• Optimum Design 50%
• Blades Design 50%
• Blade Root 50%
• Beam Element 50%