General Aviation Aircraft Design Methodology in a PC Environment 965520
A personal computer based preliminary design system for aircraft demonstrates a practical method to design and analyze any aircraft configuration. The program provides a powerful framework to support the non-unique process of aircraft preliminary design. The system will allow design engineers to rapidly evolve an aircraft configuration from weight sizing through detailed performance calculations, while working within regulatory constraints. The program is designed to reduce the preliminary design phase cost and to bring advanced design methods to small businesses and universities.
Citation: Roskam, J. and Anemaat, W., "General Aviation Aircraft Design Methodology in a PC Environment," SAE Technical Paper 965520, 1996, https://doi.org/10.4271/965520. Download Citation
Author(s):
Jan Roskam, William A. Anemaat
Affiliated:
Design, Analysis and Research Corp.
Pages: 7
Event:
World Aviation Congress & Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Business and general aviation aircraft
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