Details
| Original language | English |
|---|---|
| Number of pages | 29 |
| Publication status | Published - 2004 |
| Externally published | Yes |
Publication series
| Name | DLR-Mitteilung |
|---|---|
| Publisher | Deutschen Forschungsanstalt fur Luft-und Raumfahrt |
| ISSN (Print) | 1434-8462 |
Abstract
An overview of DLR's current research activities and results in the fields of heat transfer, thermal stresses and thermally induced buckling in composite aerospace structures is given. Novel theories and finite element formulations are presented, realistic modelling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and finally design guidelines are given.
ASJC Scopus subject areas
- Social Sciences(all)
- Transportation
- Engineering(all)
- Aerospace Engineering
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29 p. 1 ed. 2004. (DLR-Mitteilung).
Research output: Other contribution › Other publication › Research › peer review
}
TY - GEN
T1 - Models and Tools for Heat Transfer, Thermal Stresses and Stability of Composite Aerospace Structures
AU - Rolfes, R.
AU - Teßmer, J.
AU - Rohwer, K.
PY - 2004
Y1 - 2004
N2 - An overview of DLR's current research activities and results in the fields of heat transfer, thermal stresses and thermally induced buckling in composite aerospace structures is given. Novel theories and finite element formulations are presented, realistic modelling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and finally design guidelines are given.
AB - An overview of DLR's current research activities and results in the fields of heat transfer, thermal stresses and thermally induced buckling in composite aerospace structures is given. Novel theories and finite element formulations are presented, realistic modelling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and finally design guidelines are given.
UR - http://www.scopus.com/inward/record.url?scp=1542285354&partnerID=8YFLogxK
M3 - Other publication
AN - SCOPUS:1542285354
T3 - DLR-Mitteilung
ER -