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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
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
Investigations Into Glider Chassis Load Spectrum
 and    
Open Access
|Sep 2010
The Effect of a Complex Stress State on Fatigue Crack Propagation and the Orientation of the Cracking Plane in VT3-1 Aeronautical Titanium Alloy
 and    
Open Access
|Sep 2010
Numerical Models for Fatigue Crack Evolution Study
,  ,   and    
Open Access
|Sep 2010
Fatigue Damage of Rivet Joints in the Condition of Stable Cyclic Load
,   and    
Open Access
|Sep 2010
In-Service Flaw Detection and Quantification in the Composite Structures of Aircraft
 and    
Open Access
|Sep 2010
The Fatigue Life Assessment of PZL-130 Orlik Structures Based on Historical Usage Data
,   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
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels Under the Constant Amplitude and Spectrum Loadin
  
Open Access
|Sep 2010
Measurements Parameters Optimisation for X-Ray Diffractometry Measurements of Stress State Around the Rivets
  
eISSN: 2300-7591|Language: English|Publication frequency: 1 time per year
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
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