Widespread Fatigue Damage Assessment of Jet Transport Structures
Weibull Analyses of the Fatigue Life of Human Tissues
Variability of Rotor Wake Interactions and Airfoil Unsteady Aerodynamics
Validation of Life Prediction Models from Representative Testings on Aluminium Alloy Specimens
Using the Initial Flaw Concept in Current and Future Aircraft Certifications
US Air Force Risk Analysis Approach for Aging Aircraft
Unified Low Cycle Fatigue Model for Gas Turbine Engine Rotor Alloys
Uncertainty Quantification in Fatigue Lifetime Data Analysis: A Possibilistic Approach
Toward the Supportable and Durable Aircraft Fuselage Structure
Towards Weight Savings for Damage Tolerant Masts and Driveshafts
Towards automated flight-maneuver-specific fatigue analysis
Toward a Damage Tolerance Evaluation of Helicopter Composite Components
Total Fatigue Life Modeling and Data Reduction Methods (AIAA 2018-1708)
Tools for a Multiaxial Fatigue Analysis of Structures Submitted to Random Vibrations
The Use of Field Inspection Data in the Performance Measurement of Nondestructive Inspections
The Royal New Zealand Air Force Andover C.MK.1 Loads Environment Spectrum Survey (L/ESS)
The Role of Fretting Fatigue in Aircraft Rivet Hole Cracking
The Role of Corrosion Pillowing in NDI and in the Structural Integrity of Fuselage Joints
The Role of Airline's Maintenance on Continuing Airworthiness of Aging Aircraft
Thermographic NDE Application for Quantitative Disbond and Corrosion Detection in Aircraft Skin
The Mechanism of Fatigue - a Critical Factor in the Prediction of the Life of Structures
The Influence of Residual Stress on the Design and Damage Tolerance of Welded Aircraft Structures
The Impact of Forging Residual Stress on Fatigue in Aluminum (AIAA 2015-0386)
The Impact of Constitutive Modeling on Life Prediction
The Formation/Nucleation of Fatigue Cracks in Aircraft Structural Materials
The Fatigue Crack Propagation (FCP) Behavior of the Forged Mg-Zn-Y-Zr Alloy
The FAA Flight Loads Data Collection Program for Commercial Transport Aircraft
The Evolution of the BAe Hawk and its Structural Clearance
The Evaluation of a Modified Stress Intensity Factor for Cold Expanded Holes
The Effect of the Grinding Condition on Short Fatigue Crack Growth in Waspaloy at 19C
The Effect of Pressure Proof Testing on the Retardation of Multi-Site Damage
The Effect of Peening on the Life Improvement Factor of 7050 Al Alloy Aircraft Structures