General Aviation Preliminary Structural Design in a Personal Computer Environment

Paper #:
  • 971501

Published:
  • 1997-05-01
Citation:
Locke, J., Schueler, K., and Anemaat, W., "General Aviation Preliminary Structural Design in a Personal Computer Environment," SAE Technical Paper 971501, 1997, https://doi.org/10.4271/971501.
Pages:
10
Abstract:
A personal computer based preliminary structural design system has been developed for general aviation aircraft. Structural design is coupled with other elements of the preliminary design process to provide a unique and powerful framework for the preliminary design process. Capabilities include structural layout, structural weight sizing and detailed stress analysis. All of these can be applied to a number of built-in (and user defined) structural configurations. The program is designed to reduce preliminary design time and produce an efficient well-documented structural design that complies with regulatory specifications.
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