TY - GEN
T1 - Using Faceted Geometries for Analysis and Design
AU - Dannenhoffer, John F.
N1 - Publisher Copyright:
© 2024 by John F. Dannenhoffer, III. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
PY - 2024
Y1 - 2024
N2 - Many analysis and design tasks start from a previous configuration that is (unfortunately) defined by tessellated surfaces, such as in a stereo-lithography file. Sometimes these definitions come from legacy CAD tools that are no longer supported, and sometimes they come from laser scans of a real configuration (such as a wing with ice growing on the leading edge). While these files define a watertight configuration that look good in the eye-ball norm, the fact that the surfaces are faceted yields less-than-desirable results when used in CFD and FEM tools. This paper describes two techniques for transforming faceted representations into smooth boundary representations. The first, called Slugs, generates a static representation by breaking the facets into contiguous groups and then fitting each group with a B-spline; the configuration is called “static” since it cannot easily be modified, except possibly via free-form deformation tools that operate on the associated B-splines. The second, called Plugs, automatically modifies the design parameters of a user-defined parametric model to best-fit the points in the tessellated surfaces. This paper describes these two techniques and the various enhancements in them since their introduction is previous publications.
AB - Many analysis and design tasks start from a previous configuration that is (unfortunately) defined by tessellated surfaces, such as in a stereo-lithography file. Sometimes these definitions come from legacy CAD tools that are no longer supported, and sometimes they come from laser scans of a real configuration (such as a wing with ice growing on the leading edge). While these files define a watertight configuration that look good in the eye-ball norm, the fact that the surfaces are faceted yields less-than-desirable results when used in CFD and FEM tools. This paper describes two techniques for transforming faceted representations into smooth boundary representations. The first, called Slugs, generates a static representation by breaking the facets into contiguous groups and then fitting each group with a B-spline; the configuration is called “static” since it cannot easily be modified, except possibly via free-form deformation tools that operate on the associated B-splines. The second, called Plugs, automatically modifies the design parameters of a user-defined parametric model to best-fit the points in the tessellated surfaces. This paper describes these two techniques and the various enhancements in them since their introduction is previous publications.
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U2 - 10.2514/6.2024-1316
DO - 10.2514/6.2024-1316
M3 - Conference contribution
AN - SCOPUS:85194089650
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -