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  • COMPUTER PROGRAMMING AND SOFTWARE  (2)
  • Structural Mechanics; Aircraft Design, Testing and Performance  (1)
  • 1
    Publication Date: 2019-07-12
    Description: This paper describes a multi-year effort to add a structural analysis subprocess to a supersonic aircraft conceptual design process. The desired capabilities include parametric geometry, automatic finite element mesh generation, static and aeroelastic analysis, and structural sizing. The paper discusses implementation details of the new subprocess, captures lessons learned, and suggests future improvements. The subprocess quickly compares concepts and robustly handles large changes in wing or fuselage geometry. The subprocess can rank concepts with regard to their structural feasibility and can identify promising regions of the design space. The automated structural analysis subprocess is deemed robust and rapid enough to be included in multidisciplinary conceptual design and optimization studies.
    Keywords: Structural Mechanics; Aircraft Design, Testing and Performance
    Type: NASA/TM-2015-218687 , L-20529 , NF1676L-20749
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: There is a need to explore methods for reducing lengthly computer turnaround or clock time associated with engineering design problems. Different strategies can be employed to reduce this turnaround time. One strategy is to run validated analysis software on a network of existing smaller computers so that portions of the computation can be done in parallel. This paper focuses on the implementation of this method using two types of problems. The first type is a traditional structural design optimization problem, which is characterized by a simple data flow and a complicated analysis. The second type of problem uses an existing computer program designed to study multilevel optimization techniques. This problem is characterized by complicated data flow and a simple analysis. The paper shows that distributed computing can be a viable means for reducing computational turnaround time for engineering design problems that lend themselves to decomposition. Parallel computing can be accomplished with a minimal cost in terms of hardware and software.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-TM-101519 , NAS 1.15:101519 , ASME Design Technology Conferences-The Design Automation Conference; Sep 25, 1988 - Sep 28, 1988; Kissimmee, FL; United States
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: A design problem is viewed as a complex system divisible into modules. Before the design of a complex system can begin, much time and money are spent in determining the couplings among modules and the presence of iterative loops. This is important because the design manager must know how to group the modules into substems and how to assign subsystems to design teams so that changes in one subsystem will have predictable effects on other subsystems. Determining these subsystems is not an easy, straightforward process and often important couplings are overlooked. Moreover, the planning task must be repeated as new information becomes available or as the design specifications change. The purchase of this research effort is to develop a knowledge-based tool to act as an intelligent advisor for the design manager. This tool identifies the subsystems of a complex design problem, orders them into a well-structured format, and marks the couplings among the subsystems to facilitate the use of multilevel tools. The tool was tested in the decomposition of the COFS (Control of Flexible Structures) mast design which has about 50 modules. This test indicated that this type of approach could lead to a substantial savings by organizing and displaying a complex problem as a sequence of subsystems easily divisible among design teams.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-TM-101558 , NAS 1.15:101558 , International Conference on Computer Aided Optimum Design of Structures; Jun 20, 1989 - Jun 23, 1989; Southampton
    Format: application/pdf
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