16 Artikel
Uneingeschränkter Zugang | 25. Aug. 2011
Investigation into Fatigue Behaviour of Metal-Composite Glue Connection
Uneingeschränkter Zugang | 25. Aug. 2011
Experimental and Numerical Crack Initiation Analysis of the Compressor Blades Working in Resonance Conditions
Uneingeschränkter Zugang | 25. Aug. 2011
Stress Intensity Factor Analysis and Fatigue Behavior of A Crack in The Residual Stress Field of Welding
Uneingeschränkter Zugang | 25. Aug. 2011
Service Life Assessment Program of PZL-130 Orlik TCII Structure
Uneingeschränkter Zugang | 25. Aug. 2011
Monitoring of Crack Growth in a Structure Under a Composite Patch
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Uneingeschränkter Zugang | 25. Aug. 2011
The Analysis of Fatigue Crack Propagation in the Elements of Aluminum Alloy D16CZATW with a Notch in the Formof A Cylindrical Hole
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Uneingeschränkter Zugang | 25. Aug. 2011
Flight Loads Acquisition for PZL-130 Orlik TCII Full Scale Fatigue Test
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Uneingeschränkter Zugang | 25. Aug. 2011
The Effect of Electrochemical Machining on the Fatigue Strength of Heat Resistance Alloys
Uneingeschränkter Zugang | 25. Aug. 2011
Compressor Blade Fatigue Diagnostics and Modelling with the Use of Modal Analysis
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Uneingeschränkter Zugang | 25. Aug. 2011
Analysis of the Possibility to Assess the Occurrence of Hidden Corrosion in Lap Joints Using Active Thermography
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Uneingeschränkter Zugang | 25. Aug. 2011
Bonded Joint Monitoring of The Composite Aerospace Structures with The Use of Nde and Shm Approach
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Uneingeschränkter Zugang | 25. Aug. 2011
Experimental and Numerical Study of Strain Progress During and After Riveting Process for Brazier Rivet and Rivet with Compensator - Squeezing Force and Rivet Type Effect
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Uneingeschränkter Zugang | 25. Aug. 2011
Methodology of Residual Stress Measurements for Rivet Joints
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Uneingeschränkter Zugang | 25. Aug. 2011
ZL-130TCII Fracture Markers Solution for Full-Scale Fatigue Test
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Uneingeschränkter Zugang | 25. Aug. 2011
Crack Growth Analysis of the Landing Gear Pull Rod of the Fighter Jet Aircraft
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Uneingeschränkter Zugang | 25. Aug. 2011
Stress Intensity Factor Calculations for the Compressor Blade with Half-Elliptical Surface Crack Using Raju-Newman Solution
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