Synonyme wurden verwendet für:
Materialermüdung
Suche ohne Synonyme:
keywords:("Materialermüdung")
Design Parameters Influencing the Fatigue Behaviour of Riveted Lap Joints
Progress on the Pathway to a Virtual Fatigue Test
Structural Alloy Testing: Part 2—Creep Deformation and Other High-Temperature Properties
Full Scale Fatigue Testing for Mitsubishi Regional Jet
Multiple-Site Damage in Riveted Lap Joints – Experimental Observations
High Cycle Fatigue and Fatigue Crack Growth Rate in Additive Manufactured Titanium Alloys
Widespread Fatigue Damage Evaluation for Multiple Elements Based on Probabilistic Approach
Predictions of Fatigue Crack Growth and Fatigue Life for Riveted Lap Joints
Data‐Fusion NDE for Progressive Damage Quantification in Composites
Load Variation and Reliability
Multiaxial Fatigue Behavior of 30HGSA Steel Under Cyclic Tension-Compression and Reversed Torsion
Crack Initiation Location and Crack Shape Development in Riveted Lap Joints – Experimental Trends
Microstructural Characterization of Fatigue Damage of CFRP in the Veiy High Cycle Fatigue Regime
Examination of the KAWAI CLD Method for Fatigue Life Prediction of Composites
Conception of Modular Test Stand for Fatigue Testing of Aeronautical Structures
Composite Materials in Automotive Body Panels, Concerning Noise and Vibration
A Numerical Approach to the Disbonding Mechanism of Adhesive Joints
Bombardier Global 7500 Fatigue Test Cycle Rate Commissioning to ¼ Life
Comparison of Rivet Hole Expansion for Protruding Rivets; Universal and with Compensator
Rapid Calculation of Safe Acceleration Values for Aircraft Structures Under Flight Test
Weibull or Log-Normal Distribution to Characterize Fatigue Life Scatter – Which Is More Suitable?
Risks of Initial Assumptions in Fatigue and Damage Tolerance of Small Aircraft Development Programs
Full-Scale Fatigue and Residual Strength Tests of the Composite Wing Box of a Passenger Aircraft
Strain Controlled Fatigue Testing of Additive Manufactured Titanium Alloy Ti-6Al-4V
GLARE®: A Versatile Fibre Metal Laminate (FML) Concept
The birth of Arall (1945–1981)
Evaluation of a PC-9/A Wing Main Spar with Misdrills Using Enhanced Teardown at Resonance
Very High-Cycle Fatigue Characteristics of Cross-Ply CFRP Laminates in Transverse Crack Initiation
Why Should We Encourage Usage of Interference-Fit Fasteners at Airframe Structural Joints?
Automatic Differentiation of FLOWer and MUGRIDO
Fatigue Life Prediction at Cold Expanded Fastener Holes with ForceMate Bushings
Studies on the Fatigue Damage Behavior of Active Jet Engine Chevron
Effect of Strengthened Hole on the Fatigue Life of 2024-T3 Aluminum Alloy
Russian Practice to Provide Safe Operation of Airplane Structures with Long-Term Operation
Evaluating the Influence of SHM on Damage Tolerant Aircraft Structures Considering Fatigue
Effective Durability and Damage Tolerance Training: New Methods for Modern Learners
Ply Curving Termination to Suppress Delamination in Composite Ply Drop-Off