Failure analysis of aircraft tubular form-fit joints in rotating-bending fatigue tests

Engineering

• Joints (Structural Components) 100%
• Mechanical Fatigue Test 100%
• Failure Analysis 100%
• Crack Initiation 66%
• Fatigue Behavior 66%
• Scanning Electron Microscope 33%
• Fracture Morphology 33%
• Crack Propagation 33%
• Frequency Vibration 33%
• Fatigue Strength 33%
• Radial Direction 33%
• Pipeline System 33%
• Experimental Platform 33%
• Fatigue Crack Propagation 33%
• Fatigue Crack 33%
• Propagation Direction 33%
• Internal Pressure 33%
• Swaging 33%
• Internal Fluid 33%
• Multiaxial Fatigue 33%
• Service Period 33%