Details
| Original language | English |
|---|---|
| Pages (from-to) | 103-123 |
| Number of pages | 21 |
| Journal | DLR-Mitteilung |
| Issue number | 1 |
| Publication status | Published - 2004 |
| Externally published | Yes |
Abstract
The capabilities of high performance tools TRAVEST, B2000 AND CODAC were investigated. A theory which allowed for using the extended 2D-method in conjunction with four noded elements was developed. For 3D reinforced composites a new failure model was developed and implemented into TRAVEST and also studied for use in B2000, in conjunction with the 3D composite elements. The postbuckling behavior of composite panels was simulated using commercial finite element software.
ASJC Scopus subject areas
- Social Sciences(all)
- Transportation
- Engineering(all)
- Aerospace Engineering
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In: DLR-Mitteilung, No. 1, 2004, p. 103-123.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - High Performance Tools for Failure, Damage Tolerance and Stability Analysis of Composite Structures
AU - Rolfes, R.
AU - Baaran, J.
AU - Juhasz, J.
AU - Kling, A.
AU - Kuhlmann, G.
AU - Nolden, Ph
PY - 2004
Y1 - 2004
N2 - The capabilities of high performance tools TRAVEST, B2000 AND CODAC were investigated. A theory which allowed for using the extended 2D-method in conjunction with four noded elements was developed. For 3D reinforced composites a new failure model was developed and implemented into TRAVEST and also studied for use in B2000, in conjunction with the 3D composite elements. The postbuckling behavior of composite panels was simulated using commercial finite element software.
AB - The capabilities of high performance tools TRAVEST, B2000 AND CODAC were investigated. A theory which allowed for using the extended 2D-method in conjunction with four noded elements was developed. For 3D reinforced composites a new failure model was developed and implemented into TRAVEST and also studied for use in B2000, in conjunction with the 3D composite elements. The postbuckling behavior of composite panels was simulated using commercial finite element software.
UR - http://www.scopus.com/inward/record.url?scp=1442331197&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:1442331197
SP - 103
EP - 123
JO - DLR-Mitteilung
JF - DLR-Mitteilung
SN - 1434-8462
IS - 1
ER -