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Challenges Facing Design and Analysis ToolsThe design and analysis of future aerospace systems will strongly rely on advanced engineering analysis tools used in combination with risk mitigation procedures. The implications of such a trend place increased demands on these tools to assess off-nominal conditions, residual strength, damage propagation, and extreme loading conditions in order to understand and quantify these effects as they affect mission success. Advances in computer hardware such as CPU processing speed, memory, secondary storage, and visualization provide significant resources for the engineer to exploit in engineering design. The challenges facing design and analysis tools fall into three primary areas. The first area involves mechanics needs such as constitutive modeling, contact and penetration simulation, crack growth prediction, damage initiation and progression prediction, transient dynamics and deployment simulations, and solution algorithms. The second area involves computational needs such as fast, robust solvers, adaptivity for model and solution strategies, control processes for concurrent, distributed computing for uncertainty assessments, and immersive technology. Traditional finite element codes still require fast direct solvers which when coupled to current CPU power enables new insight as a result of high-fidelity modeling. The third area involves decision making by the analyst. This area involves the integration and interrogation of vast amounts of information - some global in character while local details are critical and often drive the design. The proposed presentation will describe and illustrate these areas using composite structures, energy-absorbing structures, and inflatable space structures. While certain engineering approximations within the finite element model may be adequate for global response prediction, they generally are inadequate in a design setting or when local response prediction is critical. Pitfalls to be avoided and trends for emerging analysis tools will be described.
Document ID
20010089251
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Knight, Norman F., Jr.
(Veridian Systems, Inc. Yorktown, VA United States)
Broduer, Steve
Date Acquired
August 20, 2013
Publication Date
January 2, 2001
Subject Category
Engineering (General)
Meeting Information
Meeting: FEMCI Workshop 2001: Innovative FEM Solutions to Challenging Problems
Location: Greenbelt, MD
Country: United States
Start Date: May 16, 2001
End Date: May 17, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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