NASA Langley Research Center has continued to develop its long standing computational tools to address new challenges in aircraft and launch vehicle design. This paper discusses the application and development of those computational aeroelastic tools. Four topic areas will be discussed: 1) Modeling structural and flow field nonlinearities; 2) Integrated and modular approaches to nonlinear multidisciplinary analysis; 3) Simulating flight dynamics of flexible vehicles; and 4) Applications that support both aeronautics and space exploration.


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    Title :

    Development of Advanced Computational Aeroelasticity Tools at NASA Langley Research Center


    Contributors:

    Publication date :

    2008


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English