Sensitivity Analysis for Design Optimization Integrated Software Tools, Phase I
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Sensitivity Analysis for Design Optimization...HTML
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Sensitivity Analysis for Design Optimization...HTML
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Sensitivity Analysis for Design Optimization...HTML
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Sensitivity Analysis for Design Optimization...HTML
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| Field | Value |
|---|---|
| Groups |
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| Tags |
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| isopen | False |
| license_id | us-pd |
| license_title | us-pd |
| maintainer | TECHPORT SUPPORT |
| maintainer_email | hq-techport@mail.nasa.gov |
| metadata_created | 2025-12-02T10:27:03.715713 |
| metadata_modified | 2025-12-02T10:27:03.715717 |
| notes | The objective of this proposed project is to provide a new set of sensitivity analysis theory and codes, the Sensitivity Analysis for Design Optimization Integrated Software Tool set, to work within the existing NASA O3 Tool. In this Phase I effort, the sensitivity approach will be implemented for two basic types of analysis, namely static systems of equations (linear and non-linear) and eigen-problems. This implementation will focus on the elements most commonly used for aerospace design; beam, plate, and shell elements. The following specific goals are identified: 1 Integrated Multidisciplinary Sensitivity Analysis Toolset for Design Optimization (software) 2 Use of Advanced Algorithms to Maximize Computational Efficiency (analytic sensitivities) 3 Compatibility with Existing NASA Software Design Tools for computational integration to O3. |
| num_resources | 4 |
| num_tags | 8 |
| title | Sensitivity Analysis for Design Optimization Integrated Software Tools, Phase I |