NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of analysis and design models on minimum weight designThe results of numerical experiments designed to illustrate how the minimum weight design, accuracy, and cost can be influenced by: (1) refinement of the finite element analysis model and associated load path problems, and (2) refinement of the design variable linking model are examined. The numerical experiments range from simple structures where the modelling decisions are relatively obvious and less costly to the more complex structures where such decisions are less obvious and more costly. All numerical experiments used employ the dual formulation in ACCESS-3 computer program. Guidelines are suggested for creating analysis and design models that predict a minimum weight structure with greater accuracy and less cost. These guidelines can be useful in an interactive optimization environment and in the design of heuristic rules for the development of knowledge-based expert optimization systems.
Document ID
19870002306
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salama, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ramanathan, R. K.
(Northrop Corp. Hawthorne, Calif., United States)
Schmit, L. A.
(California Univ. Los Angeles, United States)
Sarma, I. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1984
Publication Information
Publication: NASA. Langley Research Center Recent Experiences in Multidisciplinary Analysis and Optimization, Part 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
87N11739
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available