Common failures in composite structures due to through thickness loads

• Autorzy: Niklewicz, J.
• Konferencja: Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
• Języki publikacji: EN

Abstrakty

EN

The report describes a procedure for predicting the failure mode and load for a laminated curved composite beam when subjected to moment and shear loading. It shows that the necessity for detailed and expensive finite element analysis can be circumvented by the use of simple approximate methods at the preliminary design stage. This local analysis of generic flange and curved structures can be integrated into a full global analysis, or used to significantly improve 'make and test' design approaches.

Słowa kluczowe

PL

kompozyty; struktury kompozytowe; laminaty; samoloty

EN

composites; composites structures; laminates; aircrafts

• Czasopismo: Research Bulletin / Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics
• Rocznik: 2001
• Tom: nr 12
• Strony: 13-18
• Opis fizyczny: Bibliogr. 10 poz., rys., tab., wykr.

Twórcy

autor

Niklewicz, J.

• Materials Centre, National Physical Laboratory, United Kingdom