Publication Date:
2019-06-28
Description:
The 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.
Keywords:
AIRCRAFT DESIGN, TESTING AND PERFORMANCE
Type:
NASA. Langley Research Center Recent Experiences in Multidisciplinary Analysis and Optimization, Part 1; 14 p
Format:
application/pdf
