Details
| Original language | English |
|---|---|
| Pages (from-to) | 171-174 |
| Number of pages | 4 |
| Journal | Composite structures |
| Volume | 73 |
| Issue number | 2 |
| Publication status | Published - 10 Jan 2006 |
| Externally published | Yes |
Abstract
The European Commission was funding within its fifth Framework Programme the project POSICOSS, which coped with the demand to design fibre composite fuselage structures for postbuckling under ultimate load. The main objective of the work was the development of improved, fast and reliable procedures for postbuckling analysis and design of fibre composite stiffened panels of future fuselage structures. They were essential, because so far postbuckling calculations were extremely time consuming and as such not applicable for design. Another substantial objective was the creation of comprehensive experimental data bases for the purpose of validation. The Paper presents an introduction to the POSICOSS project; it derives the main objective from the main general objective for the design of the next generation of aircraft structures, and it summarizes the work done. The results achieved are only touched, because details of them can be found by consulting the references given.
Keywords
- Buckling tests, Composites, Fuselage structures, Postbuckling analysis, Stiffened panels
ASJC Scopus subject areas
- Materials Science(all)
- Ceramics and Composites
- Engineering(all)
- Civil and Structural Engineering
Cite this
- Standard
- Harvard
- Apa
- Vancouver
- BibTeX
- RIS
In: Composite structures, Vol. 73, No. 2, 10.01.2006, p. 171-174.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - POSICOSS - Improved postbuckling simulation for design of fibre composite stiffened fuselage structures
AU - Zimmermann, R.
AU - Rolfes, R.
N1 - Funding information: This work was supported by the European Commission, Competitive and Sustainable Growth Programme, Contract No. G4RD-CT-1999-00103; the funding is gratefully appreciated. The information in this paper is provided as is and no guarantee or warranty is given that the information is fit for any particular purpose. The user thereof uses the information at its sole risk and liability.
PY - 2006/1/10
Y1 - 2006/1/10
N2 - The European Commission was funding within its fifth Framework Programme the project POSICOSS, which coped with the demand to design fibre composite fuselage structures for postbuckling under ultimate load. The main objective of the work was the development of improved, fast and reliable procedures for postbuckling analysis and design of fibre composite stiffened panels of future fuselage structures. They were essential, because so far postbuckling calculations were extremely time consuming and as such not applicable for design. Another substantial objective was the creation of comprehensive experimental data bases for the purpose of validation. The Paper presents an introduction to the POSICOSS project; it derives the main objective from the main general objective for the design of the next generation of aircraft structures, and it summarizes the work done. The results achieved are only touched, because details of them can be found by consulting the references given.
AB - The European Commission was funding within its fifth Framework Programme the project POSICOSS, which coped with the demand to design fibre composite fuselage structures for postbuckling under ultimate load. The main objective of the work was the development of improved, fast and reliable procedures for postbuckling analysis and design of fibre composite stiffened panels of future fuselage structures. They were essential, because so far postbuckling calculations were extremely time consuming and as such not applicable for design. Another substantial objective was the creation of comprehensive experimental data bases for the purpose of validation. The Paper presents an introduction to the POSICOSS project; it derives the main objective from the main general objective for the design of the next generation of aircraft structures, and it summarizes the work done. The results achieved are only touched, because details of them can be found by consulting the references given.
KW - Buckling tests
KW - Composites
KW - Fuselage structures
KW - Postbuckling analysis
KW - Stiffened panels
UR - http://www.scopus.com/inward/record.url?scp=32044447885&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2005.11.041
DO - 10.1016/j.compstruct.2005.11.041
M3 - Article
AN - SCOPUS:32044447885
VL - 73
SP - 171
EP - 174
JO - Composite structures
JF - Composite structures
SN - 0263-8223
IS - 2
ER -