NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Multidisciplinary Optimization Methods for Aircraft Preliminary DesignThis paper describes a research program aimed at improved methods for multidisciplinary design and optimization of large-scale aeronautical systems. The research involves new approaches to system decomposition, interdisciplinary communication, and methods of exploiting coarse-grained parallelism for analysis and optimization. A new architecture, that involves a tight coupling between optimization and analysis, is intended to improve efficiency while simplifying the structure of multidisciplinary, computation-intensive design problems involving many analysis disciplines and perhaps hundreds of design variables. Work in two areas is described here: system decomposition using compatibility constraints to simplify the analysis structure and take advantage of coarse-grained parallelism; and collaborative optimization, a decomposition of the optimization process to permit parallel design and to simplify interdisciplinary communication requirements.
Document ID
20040161122
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Kroo, Ilan
(Stanford Univ. Stanford, CA, United States)
Altus, Steve
(Stanford Univ. Stanford, CA, United States)
Braun, Robert
(Stanford Univ. Stanford, CA, United States)
Gage, Peter
(Stanford Univ. Stanford, CA, United States)
Sobieski, Ian
(Stanford Univ. Stanford, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper -94-4325-CP
Report Number: AIAA Paper -94-4325-CP
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available