Open Access
MATEC Web Conf.
Volume 349, 2021
6th International Conference of Engineering Against Failure (ICEAF-VI 2021)
Article Number 03016
Number of page(s) 6
Section Components and Structural Elements in Engineering Applications: Design, Detections of Defects, Structural Health Monitoring
Published online 15 November 2021
  1. Šedek, J., Růžek, R., Raška, J., Bĕhal, J. Comparative study of prediction methods for fatigue life evaluation of an integral skin-stringer panel under variable amplitude loading, Procedia Engineering, 114, 2015, pp. 124-131 [CrossRef] [Google Scholar]
  2. European Aviation Safety Agency, 2010. AMC 20-29: Composite Aircraft Structure. URL: [Google Scholar]
  3. Federal Aviation Administration, Advisory Circular AC20-107B: Composite Aircraft Structure, 2010. URL:{_}Circular/AC90-114.pdf [Google Scholar]
  4. Růžek, R., Běhal, J. Certification programme of airframe primary structure composite part with environmental simulation, Int. J. of Fatigue 31(6), pp. 1073-1080 (2009) [CrossRef] [Google Scholar]
  5. European Military Airworthiness Requirements, EMAR 21 Certification of Military Aircraft and Related Products, Parts and Appliances, and Design and Production Organisations, European Defence Agency, 2018 [Google Scholar]
  6. Morton, H.J., Bishop, B.C., Clark, G. NDT of Aircraft Structures During Full-Scale Fatigue Testing, National AINDT Conference, Wollongong 1993, 6p. ISBN 0-86418-265-1 [Google Scholar]
  7. Horak, V., Novotny, D. Full Scale Fatigue Test and Failure Analysis of Advanced Jet Trainer Wing, 5th International Conference of Engineering Against Failure (ICEAF-V 2018), MATEC Web Conf. Volume 188, 2018, 9p. ISSN: 2261-236X [Google Scholar]
  8. Pascoe, J.A. Slow-growth damage tolerance for fatigue after impact in FRP composite: Why current research won’t get us there, 1st Virtual European Conference on Fracture, Procedia Structural Integrity, Volume 28, 2020, 726-733p. ISBN: 9781713824787 [CrossRef] [Google Scholar]
  9. Podstawka, M., Bělský, P. Non-destructive Inspection of L410 NG Aircraft Structure during Full-Scale Fatigue tests, 57th International Scientific Conference on Experimental Stress Analysis. Czech Society for Mechanics, Luhacovice 2019, 6p, ISBN 978-80-214-5753-9 [Google Scholar]
  10. Tserpes, K., Karachalios, E., Růžek, R., Kadlec, M. CFRP Fuselage Panel Behavior Monitoring Using Fibre Optic and Resistance Sensors and Optical Contactless Measurements. AMM 827, 51–56, 2016. [CrossRef] [Google Scholar]
  11. Belsky, P., Kadlec, M. Non-destructive Methods for Damage Assessment of Composite Sandwich Structures. MATEC Web of Conferences. 2018, 8p, ISSN: 2261-236X [Google Scholar]
  12. Kruse, T., Körwien, T., Růžek, R. Fatigue behaviour and damage tolerant design of composite bonded joints for aerospace ap-plication, Proceedings of the ECCM 2016 17th European Conference on Composite Materials ECCM-17, Munich, Germany, June 26-30, 2016. ISBN 978-300053387-7. [Google Scholar]
  13. Kruse, T., Körwien, T., Růžek, R., Hangx, R., Rans, C. Fatigue behaviour and damage tolerant design of bonded joints for aerospace application on Fibre Metal Laminates and composites, in Proc. of 29th Symposium of the International Committee on Aeronautical Fatigue (ICAF 2017), Nagoya, Japan, June 5-9, 2017, ISBN: 978-1-5108-5610-3. [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.