Design of fiber composite aerospace structures under vibration loads

Keyphrases

• Fiber Composites 100%
• Composite Aerospace Structures 100%
• Vibration Load 100%
• High Stiffness 50%
• Metal Structure 50%
• Matrix Materials 25%
• Degrees of Freedom 25%
• Polymer Matrix 25%
• Other-benefit 25%
• Vibration Behavior 25%
• Operating Conditions 25%
• Design Concept 25%
• Design Parameters 25%
• Coupling Effect 25%
• Anisotropy 25%
• Life Cycle Cost 25%
• Maintenance Effort 25%
• Design Case 25%
• Impact Resistance 25%
• Material Density 25%
• High Strength 25%
• Beneficial Properties 25%
• High Durability 25%
• Component Structure 25%
• Composite Structures 25%
• Shape-adaptive 25%
• Beneficial Use 25%
• Fatigue Durability 25%
• Temperature Damage 25%
• Bending-twisting 25%
• Fiber-reinforced Materials 25%
• Flexible Polymer 25%
• Fiber Composite Materials 25%
• Less Maintenance 25%

Engineering

• Composite Fiber 100%
• Aerospace Material 100%
• Degree of Freedom 33%
• Design Parameter 33%
• Design Concept 33%
• Lifecycle Cost 33%
• Coupling Effect 33%
• Operational Condition 33%
• Fiber Composite Material 33%
• Morphing Structure 33%
• Fibre-Reinforced Material 33%
• Impact Damage 33%
• Polymer Matrix 33%
• Matrix Material 33%
• Composite Structure 33%

Material Science

• Composite Material 100%
• Aerospace Material 100%
• Composite Material 25%
• Polymer Matrix 25%
• Density 25%
• Anisotropy 25%
• Fiber Reinforced Material 25%