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An overview of the Douglas Aircraft Company Aeroelastic Design Optimization Program (ADOP)From a program manager's viewpoint, the history, scope and architecture of a major structural design program at Douglas Aircraft Company called Aeroelastic Design Optimization Program (ADOP) are described. ADOP was originally intended for the rapid, accurate, cost-effective evaluation of relatively small structural models at the advanced design level, resulting in improved proposal competitiveness and avoiding many costly changes later in the design cycle. Before release of the initial version in November 1987, however, the program was expanded to handle very large production-type analyses.
Document ID
19890015850
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dodd, Alan J.
(McDonnell-Douglas Corp. Long Beach, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Recent Advances in Multidisciplinary Analysis and Optimization, Part 3
Subject Category
Aircraft Design, Testing And Performance
Accession Number
89N25221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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