Flexible Software Environment for the Coupled Aerothermodynamic-Thermal Analysis of Structures

Details Flexible Software Environment for the Coupled Aerothermodynamic-Thermal Analysis of Structures Flexible Software Environment for the Coupled Aerothermodynamic-Thermal Analysis of Structures

Feb 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..263h&link_type=abstract

Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,

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This article describes a simulation environment for the coupled thermal and mechanical analysis of spacecraft structures. The numerical concept bases on the weak form of the interface conditions on the coupling surface. The iterative solution of the coupled equations is done with the classical Dirichlet-Neumann approach. Transient problems are handled with staggered schemes. The software environment combines existing fluid and structural analysis codes. Aspects of the architecture and its implementation are described. Finally an application to a spacecraft structure is shown.

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