Mixed time integration methods for transient thermal analysis of structures are studied. An efficient solution procedure for predicting the thermal behavior of aerospace vehicle structures was developed. A 2D finite element computer program incorporating these methodologies is being implemented. The performance of these mixed time finite element algorithms can then be evaluated employing the proposed example problem.
Mixed time integration methods for transient thermal analysis of structures, appendix 5
1982-01-01
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English
Transient thermal analysis of Vega launcher structures
Tema Archive | 2008
|Appendix D Numerical Integration
AIAA | 1999
|Appendix B: Integration Techniques
AIAA | 2007
|