An interactive system for aircraft design and optimizationA system for aircraft design utilizing a unique analysis architecture, graphical interface, and suite of numerical optimization methods is described in this paper. The non-procedural architecture provides extensibility and efficiency not possible with conventional programming techniques. The interface for analysis and optimization, developed for use with this method, is described and its application to example problems is discussed.
Document ID
19920050678
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kroo, Ilan M. (Stanford University CA, United States)