Applications to fixed-wing aircraft and spacecraftAerospace-industry applications of general-purpose structural optimization codes have not progressed as far as they might due to the lack of preprocessor capabilities. With the emergence of a new generation of graphic preprocessors that are capable of creating design models, these methods will gain acceptance. Attention is given to recent innovative applications of the Flutter and Strength Optimization Program and TSO, and the role of structural optimization in a multidisciplinary design system. Illustrative aircraft structure examples are used throughout the presentation.
Document ID
19930061435
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Miura, Hirokazu (NASA Ames Research Center Moffett Field, CA, United States)
Neill, Douglas J. (Northrop Corp. Aircraft Div., Hawthorne, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publisher: American Institute of Aeronautics and Astronautics, Inc.