NASA NTRS · 19910047596
General shape optimization capability
Abstract
A method is described for calculating shape sensitivities, within MSC/NASTRAN, in a simple manner without resort to external programs. The method uses natural design variables to define the shape changes in a given structure. Once the shape sensitivities are obtained, the shape optimization process is carried out in a manner similar to property optimization processes. The capability of this method is illustrated by two examples: the shape optimization of a cantilever beam with holes, loaded by a point load at the free end (with the shape of the holes and the thickness of the beam selected as the design variables), and the shape optimization of a connecting rod subjected to several different loading and boundary conditions.
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Chargin, Mladen K., Raasch, Ingo, Bruns, Rudolf, Deuermeyer, Dawson. 1991-02-01. General shape optimization capability. https://ntrs.nasa.gov/citations/19910047596
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