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Volume 2009 (2009): Issue 1 (Jul 2009)

Open Access
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Fatigue of Aircraft Structures
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Issue 1 (July 2009)
19 articles
Open Access
|Sep 2010
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin
  
Open Access
|Sep 2010
Capacity of Fractographic Analysis for Load-Time History Reconstruction and Fatigue Crack Growth Rate Estimation for the 2024-T3 Aluminium Alloy
,   and    
Open Access
|Sep 2010
In-Service Flaw Detection and Quantification in the Composite Structures of Aircraft
 and    
Open Access
|Sep 2010
Numerical Models for Fatigue Crack Evolution Study
,  ,   and    
Open Access
|Sep 2010
The Rivet Parameter Influence in Fatigue Strength
,  ,   and    
Open Access
|Sep 2010
Measurements Parameters Optimisation for X-Ray Diffractometry Measurements of Stress State Around the Rivets
  
Open Access
|Sep 2010
Fatigue Damage of Rivet Joints in the Condition of Stable Cyclic Load
,   and    
Open Access
|Sep 2010
Strength Testing and Analysis of Fatigue Crack Growth in Selected Aircraft Materials
 and    
Open Access
|Sep 2010
Analysing Micromechanisms of Initiation and Propagation of Short Fatigue Cracks from Rivet Holes in the Aluminums Sheets
 and    
Open Access
|Sep 2010
Deterministic Approach to Predicting the Fatigue Crack Growth in the 2024-T3 Aluminum Alloy Under Variable Amplitude Loading
 and    
eISSN: 2300-7591|ISSN: 2081-7738|Language: English
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Related subjects:
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