Concept for a deployable wing

Engineering

• Finite Element Modeling 100%
• Snap-Through 50%
• Analytical Model 50%
• Leading Edge 50%
• Bending Tests 50%
• Static Analysis 50%
• Bending Stiffness 50%
• Trailing Edge 50%
• Glass Fibre-Reinforced Plastic Composite 50%
• Suction Side 50%
• Regular Interval 50%
• Unmanned Aircraft 50%
• Pressure Side 50%
• Maximum Bending Moment 50%

Material Science

• Finite Element Modeling 100%
• Aircraft 50%
• Snap-Through 50%
• Glass Fiber Reinforced Plastics 50%
• Bending Moment 50%