Details
| Original language | English |
|---|---|
| Pages (from-to) | 125-153 |
| Number of pages | 29 |
| Journal | DLR-Mitteilung |
| Issue number | 1 |
| Publication status | Published - 2004 |
| 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 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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In: DLR-Mitteilung, No. 1, 2004, p. 125-153.
Research output: Contribution to journal › Review 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 - 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 - Review article
AN - SCOPUS:1542285354
SP - 125
EP - 153
JO - DLR-Mitteilung
JF - DLR-Mitteilung
SN - 1434-8462
IS - 1
ER -