Stress - Intensity Factor Solutions for Cracks at Countersunk Rivet Holes under Uniaxial Tension
A Study on Engineering Small Crack Growth under both Elastic and Elasto-Plastic Conditions
CF116 (CF-5) Full Scale Durability and Damage Tolerance Test (FSDATT)
Application of Full Scale Test Results to Structural Modification
Reliable Stress and Fracture Mechanics Analysis of Complex Aircraft Components
CF116 Upper Wing Skin Compression Induced Fatigue Cracking: A Case Study
Probabilistic Durability Analysis Methodology for Metallic Airframes
Influence of Initial Defect Conditions on Structural Fatigue in RAAF Aircraft
Practical Evaluation of Crack Detection Capability for Visual Inspection in Japan
Calculation Method for Predicting the Fatigue Life of Riveted Joints
Thermographic NDE Application for Quantitative Disbond and Corrosion Detection in Aircraft Skin
Evaluation of Current Analytical Methods for Crack Growth in a Bolt
Mean Stress Models for Low Cycle Fatigue of a Nickel-Base Super Alloy
Fatigue Life and Bird Strike Resistance of a Composite Fan Blade for Advanced Ducted Engines
CF-18 Fighter FS 488 Bulkhead Post-ECP 45/320 Flight Strain Survey
Correlation Between Material Properties and Damage Tolerance Behaviour of Composite Structures
Design Parameters and Variability in the Aircraft Sizing Process - Aspects of Damage Tolerance
Optimum Aircraft Structural Design and Verification for Users