Details
| Original language | English |
|---|---|
| Pages (from-to) | 641-670 |
| Number of pages | 30 |
| Journal | Journal of thermal stresses |
| Volume | 26 |
| Issue number | 6 |
| Publication status | Published - Jun 2003 |
| Externally published | Yes |
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 modeling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and design guidelines are given.
Keywords
- Composites, Fiber Metal Laminates, Heat Transfer, Hybrid Structures, Thermal Buckling, Thermal Stresses
ASJC Scopus subject areas
- Materials Science(all)
- General Materials Science
- Physics and Astronomy(all)
- Condensed Matter Physics
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In: Journal of thermal stresses, Vol. 26, No. 6, 06.2003, p. 641-670.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
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 - 2003/6
Y1 - 2003/6
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 modeling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and 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 modeling of boundary conditions and junction areas is highlighted, experimental validation is discussed, and design guidelines are given.
KW - Composites
KW - Fiber Metal Laminates
KW - Heat Transfer
KW - Hybrid Structures
KW - Thermal Buckling
KW - Thermal Stresses
UR - http://www.scopus.com/inward/record.url?scp=0242526873&partnerID=8YFLogxK
U2 - 10.1080/713855951
DO - 10.1080/713855951
M3 - Article
AN - SCOPUS:0242526873
VL - 26
SP - 641
EP - 670
JO - Journal of thermal stresses
JF - Journal of thermal stresses
SN - 0149-5739
IS - 6
ER -