Abstract
The use of displacements as design variables for truss structure optimization is considered as an alternative to the conventional, nested FE analysis based design approach. A two level optimization has been developed; in an inner level, cross sectional areas of truss members are designed for a given displacement field, and in an outer level, optimal displacements are searched trough the use of sequential linear programming. The efficiency and the speed of the method are shown by two test examples for some weight minimization. The evolution of the areas and of the weight is studied. Beside the efficiency of the method, one of the main conclusion is that the weight is always continuous trough the design history although areas might exhibits large discontinuities.
Original language | English (US) |
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Pages | 681-690 |
Number of pages | 10 |
DOIs | |
State | Published - 1998 |
Externally published | Yes |
Event | 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1998 - St. Louis, United States Duration: Sep 2 1998 → Sep 4 1998 |
Other
Other | 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1998 |
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Country/Territory | United States |
City | St. Louis |
Period | 9/2/98 → 9/4/98 |
ASJC Scopus subject areas
- Aerospace Engineering
- Mechanical Engineering