A novel design for reinforcing the aircraft tail leading edge structure against bird strike

Engineering

• Leading Edge Structure 100%
• Deformation Behavior 33%
• Finite Element Analysis 33%
• Experimental Result 33%
• Simulation Result 33%
• Good Agreement 33%
• Numerical Model 33%
• Leading Edge 33%
• Aircraft Structure 33%
• Damage Behavior 33%
• Commercial Aircraft 33%
• Effective Mean 33%