The field of thermomechanical activities of the Institute for Structural Mechanics in numerical and experimental analysis of aerospace structures is presented. After discussing the implications and prerequisites, knowledge of load spectra and material characteristics, structural concepts for heat protection during reentry, orbital application, and use of carbon fiber reinforced polymers in airplanes are examined. From these concepts the tasks of thermal and structural analysis as well as the testing requirements are deduced.
Thermomechanics Tasks and Applications
1990
24 pages
Report
No indication
English
Manned Spacecraft , Aircraft , Composite Materials , Engineering Materials , Carbon fiber reinforced plastics , Loads (Forces) , Structural analysis , Thermal analysis , Thermomechanical treatment , Couplings , Structural engineering , Thermal protection , Thermodynamics , Foreign technology , Spacecraft construction materials , Aircraft construction materials , Design criteria
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