General Aviation Preliminary Structural Design in a Personal Computer Environment 971501
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.
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. Download Citation
Author(s):
James Locke, Kurt L. Schueler, William A. Anemaat
Affiliated:
Design, Analysis and Research Corp.
Pages: 10
Event:
SAE General, Corporate and Regional Aviation Meeting and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Business and general aviation aircraft
Design processes
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