Prediction of fatigue damage in tapered laminates

Engineering

• Acceptable Limit 33%
• Bending Effect 33%
• Blades Design 33%
• Crack Density 33%
• Damage Initiation 33%
• Damage-Tolerant Design 33%
• Failure Criterion 33%
• Failure Initiation 33%
• Fatigue Damage 100%
• Fatigue Failure 33%
• Give Rise 33%
• Laminate 100%
• Loading Cycle 33%
• Mechanisms 33%
• Multiaxial Stress State 33%
• Remaining Life 33%
• Stress Level 33%
• Stress State 33%