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Materialermüdung
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keywords:("Materialermüdung")
Design of composite structures against fatigue : applications to wind turbine blades
High cycle fatigue in aircraft gas turbines - an industry perspective
Development of an on-board fatigue processor for helicopters
A study of wheel-rail contact, wear and cummulative damage
Fatigue damage calculation in stress concentration fields under variable uniaxial stress
A growth model for catastrophic cracking in an RAAF aircraft
Prevention of fatigue failures in elastic coupling discs and in fan blades
Semi designed for conversion to drilling/production unit
Probalistic prediction of extreme stress and fatigue damage for ships inslamming conditions
The shape optimisation of a connecting rod with fatigue life constraint
A Probabilistic Approach to Aircraft Structures Risk Assessment
Analytical Predictions of the Residual Strength of Graphite Fiber-Reinforced Laminated Composites
Fatigue Life Predictions for Notch Geometries in a Gas Turbine Disc Material
Statistical Analysis of Fatigue Behaviour of Aluminium Alloys in the Presence of Prior Corrosion
Fatigue and Damage Tolerance of Ageing Aircraft Structures
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
A Monte-Carlo Approach for the Assessment of Widespread Fatigue Damage in Aircraft Structures
Riveted Lap Joints of the Fiber Metal Laminate GLARE under Biaxial Loading
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
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