Body freedom flutter study and passive flutter suppression for a high aspect ratio flying wing model

Engineering

• High Aspect Ratio 100%
• Mass Balance 100%
• Design Optimization 50%
• Normal Mode 50%
• Design Parameter 50%
• Bending Stiffness 50%
• Sweep Angle 50%
• Parametric Study 50%
• Parametric Analysis 50%
• Critical Flutter Speed 50%