Abstract
Many engineering problems are associated with both continuous and discrete design parameters. While continuous optimization procedures are well established and discrete techniques are becoming more widely used, there is a need for the development of methods which can appropriately include both types of variables. This paper presents a hybrid optimization technique which incorporates continuous and discrete design variables simultaneously. A simulated annealing algorithm is used in conjunction with a gradient based search in the formulation. Numerical examples are presented to demonstrate the procedure. In the first, the mass of a ten bar truss is minimi/,ed using continuous parameters and discrete variables which are allowed to vary from within a set of preselected values. Results indicate that the hybrid optimization procedure produces a better optimum in fewer iterations compared to other existing techniques when applied to a ten bar truss mass minimization. An application to maximize the buckling load of a composite cylinder is also presented.
Original language | English (US) |
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Title of host publication | 6th Symposium on Multidisciplinary Analysis and Optimization |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
Pages | 1430-1440 |
Number of pages | 11 |
State | Published - 1996 |
Event | 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1996 - Bellevue, United States Duration: Sep 4 1996 → Sep 6 1996 |
Other
Other | 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1996 |
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Country/Territory | United States |
City | Bellevue |
Period | 9/4/96 → 9/6/96 |
ASJC Scopus subject areas
- Aerospace Engineering
- Mechanical Engineering