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Volume 2017 (2017): Issue 9 (Dec 2017)

Open Access
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Fatigue of Aircraft Structures
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Issue 9 (December 2017)

12 articles
Open Access
|Aug 2018
Identification of Delamination in Composite Beams using the Fractal Dimension-Based Damage Identification Algorithm
 and    
Open Access
|Aug 2018
Localization of Sound Sources during Full Scale Fatigue Test of the Vertical Stabilizer with the Acoustic Holography Technique
  
Open Access
|Aug 2018
Calibration of the Ductile Failure Criterion for Nickel-Based Superalloys taking into Account the Localization of the Strain
 and    
Open Access
|Aug 2018
Methods for Different Orders Stresses Estimation with Diffraction Methods
  
Open Access
|Aug 2018
Enhancement of Damage Detectability in Aircraft Structures Using the Fusion of NDT Results
,   and    
Open Access
|Aug 2018
Evaluation of the Suitability of the Strain-Gauge Method for Measuring Deformations during the Fatigue Tests of Aviation Composite Structures
 and    
Open Access
|Aug 2018
Study on Possible Replacement of the Aluminum Spar with a Composite Structure Illustrated with the Case of Agricultural Aircraft
,   and    
Open Access
|Aug 2018
Introduction of an Individual Aircraft Tracking Program for the Polish SU-22
,  ,  ,   and    
Open Access
|Aug 2018
The Effect of Anodizing Process Parameters on the Fatigue Life of 2024-T-351-Aluminium Alloy
 and    
Open Access
|Aug 2018
A Model for Fatigue Crack Growth in the Paris Regime under the Variability of Cyclic Hardening and Elastic Properties
,   and    
eISSN: 2300-7591|ISSN: 2081-7738|Language: English
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
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