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The Role of Corrosion Pillowing in NDI and in the Structural Integrity of Fuselage Joints
Numerical `Round Robin' Tests on the Assessment of MSD
Operational Loads and Usage Monitoring: The ASH-37 Solution for Flight Data Analysis
Repair Assessment Program for Airbus A300 Aircraft
EH 101 Airframe - The Fatigue Testing and Resulting Timely Modifications for the Production Aircraft
Fatigue Strength of Fuselage Joint Structures under Ambient and Corrosive Environment
An Assessment of the Probability of Failure Associated with the Use of a Life Factor of Two
Enhancements to Repair Assessment and Integrated Design (RAPID)
Impacting Thin Skinned Composite Sandwich Laminates
Fatigue Crack Closure and Fatigue Thresholds
Making Fuselage Riveted Lap Splices with 200-Year Crack-Free Fatigue Lives
Eurofighter 2000: An Integrated Approach to Structural Health and Usage Monitoring
T~e^* as a Low-Cycle Fatigue Crack Growth Parameter
Effects of Combined Loads on the Nonlinear Response of Stiffened Shells with Long Cracks
Durability Issues in Bonded Joint Design
Effects of Low-Amplitude Cycles in Spectrum Loading on a Fighter Aircraft
The Alphajet Life Extension Program
An Evaluation of Damage Tolerance Characteristics of Sandwich Composite Structures
The Characteristics of Multi-Site Fatigue Damage in the Fuselage Riveted Lap Splice Joint
The Role of Fretting Fatigue in Aircraft Rivet Hole Cracking
Residual Stress Analysis of Cold Expanded Bushings
Crack Turning Damage Tolerance Approach for Integrally Stiffened Structure
Fatigue Crack Retardation in Aluminium Alloys by Means of Squeeze Dimpling
Fatigue Damage Design Principles of Fibre-Reinforced Titanium Matrix Composites
A comparison of 2024-T3 and 2524-T3 Aluminium Alloys under Multi-Site Damage Scenarios
Sample size determination of bogey tests without failures
Corrosion of aluminum alloy in aircraft fuel tank compartments due to condensed water
Influence of Thickness on Crack Growth Life of Coldworked Holes
Fatigue-Life Prediction of Riveted Lap-Splice Joints using Small-Crack Theory
Lessons Learned from the C17A Full Scale Airframe Durability Qualification Test Program
Delamination Behavior of Spliced Fiber Metal Laminates
Probability Modelling of Corrosion Fatigue Crack Growth and Pitting Corrosion
Recovery of the RAAF Macchi MB326H - The Talc of an Aging Trainer Fleet
Ageing Aircraft USAF Experience and Actions
Statistics of Aircraft Accidents and Case Studies on Structure or Material Related Accidents
Full Scale GLARE Fuselage Panel Tests
Boundary Element Methods for Damage Tolerance Analysis of Aircraft Panels
Evaluation of locomotive cable insulation life under varying temperature loading