Structural Optimization via Steepest Descent and Interactive Computation
Item
- Title
- Structural Optimization via Steepest Descent and Interactive Computation
- Description
- In this paper a hybrid method of optimal structural design is developed and applied, using a steepest descent optimization technique in an interactive mode of computing. A method of computing design sensitivity is developed as part of a steepest descent optimization method. A technique is presented for utilization of this data by an experienced designer, interacting with the iterative computer algorithm. The designer is allowed to alter the structural configuration to seek a global, rather than just a local, optimum. Two examples are solved with a number of loading conditions and design constraints to illustrate the flexibility of the technique. Results for these problems are of interest in their own right.
- Creator
- Haug, E. J., Jr.
- Arora, J. S.
- Abstract
- In this paper a hybrid method of optimal structural design is developed and applied, using a steepest descent optimization technique in an interactive mode of computing. A method of computing design sensitivity is developed as part of a steepest descent optimization method. A technique is presented for utilization of this data by an experienced designer, interacting with the iterative computer algorithm. The designer is allowed to alter the structural configuration to seek a global, rather than just a local, optimum. Two examples are solved with a number of loading conditions and design constraints to illustrate the flexibility of the technique. Results for these problems are of interest in their own right.
- Corporate Author
- University of Iowa
- Report Number
- AFFDL TR 71-160 p. 591-618
- Report Availability
- Full text available
- Publisher
- Wright-Patterson Air Force Base, OH : Air Force Flight Dynamics Laboratory, Air Force Systems Command and Air Force Institute of Technology, Air University
- Date
- 1973
- Type
- article
- Date Issued
- 1973-12
- Provenance
- Bombardier/Aero
- Distribution Classification
- 1
- Distribution Conflict
- No
- DTIC Record Exists
- No
- Format
- 1 online resource (28 pages) : ill.
- Extent
- 28
- Identifier
- AD0785968
Linked resources
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Title | Class |
---|---|
Proceedings of the Third Conference on Matrix Methods in Structural Mechanics: Proceedings of the Conference held at Wright-Patterson Air Force Base, Ohio 19-21 October 1971 |