A composites optimization capability for aircraft engine components, for structural and thermal design requirements, is currently under development. A heat transfer analysis is coupled to a structural analysis by using the heat transfer results, in terms of the nodal temperatures, in the structural solution. The multidiscipline optimization capability includes provision for providing multiple objective functions and a capability for approximation of the gradients. Several realistic aircraft engine components are optimized for structural, thermal, and/or aeromechanical responses as design objectives and constraints.


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    Title :

    Optimization of composite engine structures for mechanical and thermal loads


    Additional title:

    Die Optimierung von Verbundstrukturen in Triebwerken für mechanische und thermische Belastungen


    Contributors:


    Publication date :

    1993


    Size :

    9 Seiten, 7 Bilder, 2 Tabellen, 12 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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