The strength and stiffness design process is described in terms of its constituents. An integrated structural analysis and design system developed at Boeing, ATLAS, is described in terms of its system architecture and its technical capabilities and examples of its use are given. Finally, the basic motivation for the development of such analysis tools and the impact of design automation are considered.
Aircraft strength and stiffness design automation
Automation bei der Bestimmung der Flugzeugstaerke und Steifigkeit
1975
11 Seiten, 15 Bilder, 2 Tabellen, 3 Quellen
Conference paper
English
Automation of the aircraft design process
NTRS | 1974
|Variable-stiffness damping aircraft landing gear and aircraft
European Patent Office | 2025
|ATC Automation 1 - Aircraft and ATM automation
Online Contents | 2006
|Aircraft wing design automation with ESO and GESO
Automotive engineering | 2002
|