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Rissausbreitung
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Bulging Factor Solutions for Cracks in Longitudinal Lap Joints of Pressurized Aircraft Fuselages
Crack Growth Retardation Model Using an Effective Stress Concept
Crack Growth Behavior of 2219-T87 Aluminum Alloy from 20 K (-423 F) to 422 K (300 F)
Investigating the Constraint Effect in a Particulate Composite Material
Development of Advanced Life Prediction Tools for Elastic-Plastic Fatigue Crack Growth
Structural Risk Assessment of RAAF B707 Lower Wing Stringers
Residual Strength Test on Stiffened Panels with Multiple-Site Damage
The Effect of Load Sequence on Fatigue Crack Propagation under Random Loading and Program Loading
Overview of Fatigue and Damage Tolerance Performance of Powder Bed Fusion Alloy N07718
Fracture Mechanics Research at Air Force Research Laboratory
Biaxial Strength of M I G-Welded and T I G- Welded 2014- T6 at 70 Deg, -320 Deg and -423 F
Investigation of Current Methods to Identify Helicopter Gear Health
Overview of Fatigue and Damage Tolerance Performance of SLM Alloy 718
Effect of Loading Frequency on the Strain Behavior and Damage Accumulation in Low-Cycle Fatigue
Survey of Serious Aircraft Accidents Involving Fatigue Fracture. Volume 2: Rotary-Wing Aircraft
Aircraft Structural Fatigue. Proceedings of a Symposium held in Melbourne, 19-20 October, 1976
Failure Criteria for Viscoelastic Materials Quarterly Progress Report, 1 Mar. - 31 Aug. 1969
Survey of Serious Aircraft Accidents Involving Fatigue Fracture. Volume 1: Fixed-Wing Aircraft
Prediction of Crack Initiation and Growth in Solid Propellants