Rolfes, R. and Tacke, S. and Zimmermann, R. (1999) Development and Experimental Verification of FE-Model for Stringer-Stiffened Fibre Composite Shells under Combined Thermal and Mechanical Loading Conditions. In: European Conference on Spacekraft Structures, Materials and Mechanical Testing, SP 428, pp. 109-115. ESA Publications Division. European Conference on Spacecraft Structures, Materials and Mechanical Testing, Braunschweig, 4.-6.11.1998. ISBN 92-9092-712-7.
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In this paper a buckling design rule for stringer stiffened curved CFRP panels subjected to combined mechanical and thermal loading is derived by parametric studies with the finite element system ANSYS. At first a finite element model to simulate the buckling behaviour of such panels is established and validated with test results from a former study. Then loading and boundary conditions are adapted to those of the Thermex B testing site at DLR in Braunschweig, and results of linear bifurcation analyses with constant material properties under combined mechanical and thermal load are presented. Additional nonlinear computations with temperature dependent material properties confirm the results of the linear computations. The results of all computations are summarized as the design rule looked for, and then verified by tests.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1999, monograph_id=SM98-046/222,|
|Title:||Development and Experimental Verification of FE-Model for Stringer-Stiffened Fibre Composite Shells under Combined Thermal and Mechanical Loading Conditions|
|Journal or Publication Title:||European Conference on Spacekraft Structures, Materials and Mechanical Testing|
|Page Range:||pp. 109-115|
|Publisher:||ESA Publications Division|
|Event Title:||European Conference on Spacecraft Structures, Materials and Mechanical Testing, Braunschweig, 4.-6.11.1998|
|Organizer:||CNES, DLR, ESA|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik|
|Deposited By:||Sibylle Wolff|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 14:37|
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