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Materialermüdung
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Fatigue Analysis of the Compressor Blades with V- Notches
Statistical Analysis of Fatigue Crack Growth Based on the Unigrow Model
Experimental and Numerical Study of Stress and Strain Field around the Rivet
A Unified Variable-Amplitude Model for Crack Initiation and Crack Propagation
Formation of a Metal Coating by Means of Friction Stir Processing
A320 ESG Full Scale Fatigue Test - Lessons Learned
Cyclic Stress-Strain and Strain-Life Properties of Aerospace Metallic Materials
Improvements in Fatigue Evaluations of Helicopter Transmissions
Damage Tolerance for Composite Parts
Durability and Damage Tolerance Evaluation of VaRTM Composite Wing Structure
Crack Growth Rate Curves: Which Part Dominates Life Prediction and When?
Fatigue Life of Cold Expanded Fastener Holes at Short Edge Margins
Analysis of Requirements on Fatigue and Damage Tolerance for Civil Transport Airplanes
Integrated Probabilistic Analysis of Damage Tolerance and Risk for Airframe Structural Locations
Link between Flight Maneuvers and Fatigue
Fatigue Life Estimation of Structures Subjected to Vibratory Loading
The Formation/Nucleation of Fatigue Cracks in Aircraft Structural Materials
Fatigue Life Assessment for Composite Structure
Recent Development on Bonded Structures
Fatigue Life Improvement Using In-situ Robotic Processes
Fatigue Life Improvement of Metallic Aerospace Structures via Crenellations
Benefits of Using a Risk Process in ASIP - The CF-18 Experience
A Structural Defect Expansion Model Based on Physical Correlation
Critical Distance for Fatigue Life Prediction in Aerospace Materials
Fatigue Analyses of Riveted Lap-Splice Joints in a Narrow-Body Aircraft
Modelling of Continuing Damage for Damage Tolerance Analysis
Fatigue Damage Behavior of Glass/Epoxy Composites Using Carbon Nanotubes as Sensors
NH90 Qualification According to Damage Tolerance
Development of a New Fiber Metal Laminate Variant Optimized for Cold Expansion and Riveting of Holes
Fleet Recovery and Life Extension - Some Lessons Learned
Damage Tolerance of Titanium Alloy Rotorcraft Components: Advantages and Challenges