1. Numerical evaluation of barely visible impact damage in a carbon fibre-reinforced composite panel with shear loading;Šedek,2017
2. EASA, 2010. European Aviation Safety Agency, AMC 20-29: Composite Aircraft structures, Annex II-AMC 20-29 to ED Decision 2010/003/R.
3. FAA, 2016. Federal Aviation Administration, AAWG Structural Damage Capability Recommendation Document, Initial Revision.
4. Certification programme of airframe primary structure composite part with environmental simulation Int. J;Růžek;of Fatigue, Volume,2009
5. Kruse, T., Körwien, T., Růžek, 2016. R. Fatigue behaviour and damage tolerant design of composite bonded joints for aerospace ap-plication, Proceedings of the ECCM 17th European Conference on Composite Materials ECCM-17, Munich, Germany.