Gust response of an elasto-flexible morphing wing using fluid–structure interaction simulations

Keyphrases

• Aspect Ratio 33%
• Cosine 33%
• Deformable Membrane 33%
• Deformation Measurement 33%
• Elastic Membrane 66%
• Flexible Membrane 33%
• Flight Characteristics 33%
• Flight Environment 33%
• Flow Field 33%
• Flow Field Measurement 33%
• Flow-induced Deformation 33%
• Fluid-structure Interaction 100%
• Gust 66%
• Gust Loads 33%
• Gust Response 100%
• High-lift 33%
• Interaction Simulation 100%
• Intermediate Configuration 33%
• Lift Coefficient 33%
• Lifting Surface 33%
• Low Reynolds number 33%
• Maximum Amplitude 33%
• Morphing Wing 100%
• Numerical Results 66%
• Peak Load 33%
• ReAttach 33%
• Root Bending Moment 33%
• Separation Behavior 33%
• Unmanned Aircraft 33%
• Wing Loading 33%
• Wing Model 33%

Engineering

• Aspect Ratio 50%
• Bending Moment 50%
• Elastic Membrane 100%
• Flow Distribution 100%
• Good Agreement 50%
• Gust Loads 50%
• Intermediate Configuration 50%
• Lift Coefficient 50%
• Lifting Surface 50%
• Main Difference 50%
• Peak Load 50%
• Rigid Wings 50%
• Unmanned Aircraft 50%