A Rapid Geometry Engine for Preliminary Aircraft Design
نویسنده
چکیده
A rapid geometry engine (RAGE) has been developed to allow for preliminary design analysis without labor-intensive CAD support. The geometry tool builds complex aircraft configurations using a component-based approach. Basic algorithms for creating the primary components are presented and discussed. Examples of many widely varying geometry models are shown. A select geometry model is analyzed with several aerodynamic analysis methods ranging in fidelity to further demonstrate the versatility of the geometry tool. Example uses of the tool in optimization problems are also presented. Future plans for the geometry engine are also discussed.
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