High fidelity trim calculation under consideration of aeroelastic effects of a high aspect ratio swept wing

Keyphrases

• High Aspect Ratio 100%
• Aeroelastic Effect 100%
• Swept Wing 100%
• Highly Accurate 50%
• Fluid-structure Interaction 50%
• Aircraft Wing 50%
• Overall Behaviors 50%
• Aircraft Model 50%
• Interaction Techniques 50%
• Wing Design 50%
• Computational Fluid 50%
• Morphing Structures 50%
• Transport Aircraft 50%
• Active Load 50%
• High Aspect Ratio Wing 50%
• Composite Wing 50%
• Passive Load 50%
• Load Behavior 50%

Engineering

• Swept Wings 100%
• Aeroelastic Effect 100%
• High Aspect Ratio 100%
• Wings 33%
• Aircraft Model 33%
• Morphing Structure 33%
• Transport Aircraft 33%
• Active Load 33%
• Fluid-Structure Interaction 33%