Contact-aided compliant mechanisms for morphing aircraft skin

Keyphrases

• Contact-aided Compliant Mechanism 100%
• Morphing Aircraft 100%
• Structural Mass 100%
• Aircraft Skin 100%
• Deflection 50%
• Non-contact 50%
• Nonlinear Elasticity 50%
• Stress-strain 50%
• Induced Stress 50%
• Linear Elastic 50%
• Multilinear 50%
• Stress Relief 50%
• Sandwich Structure 50%
• Contact Structure 50%
• Contact-aided 50%
• Contact Mechanism 50%
• Maximum Stress 50%
• Aerodynamic Loads 50%
• Material Model 50%
• Small UAV 50%
• Honeycomb Structure 50%
• Global Strain 50%
• Material Reduction 50%
• Global Maximum 50%
• Linearly Elastic Material 50%

Engineering

• Compliant Mechanism 100%
• Aircraft 100%
• Induced Stress 50%
• Unmanned Aerial Vehicle 50%
• Stress Relief 50%
• Honeycomb Structure 50%
• Aerodynamic Load 50%
• Maximum Stress 50%
• Material Model 50%
• Nonlinear Elastic Material 50%
• Sandwich Structures 50%

Material Science

• Aircraft 100%
• Elastic Material 100%
• Compliant Mechanism 100%
• Honeycomb Structure 50%