Title:
Potential Formulation for Aeroelastic Constraint Analysis in a Conceptual Design Environment
Potential Formulation for Aeroelastic Constraint Analysis in a Conceptual Design Environment
| dc.contributor.author | De Baets, Peter Wilfried Gaston | en_US |
| dc.contributor.author | Mavris, Dimitri N. | en_US |
| dc.contributor.corporatename | American Institute of Aeronautics and Astronautics | |
| dc.contributor.corporatename | Georgia Institute of Technology. Aerospace Systems Design Laboratory | |
| dc.date.accessioned | 2005-05-26T13:59:02Z | |
| dc.date.available | 2005-05-26T13:59:02Z | |
| dc.date.issued | 2002-04 | en_US |
| dc.description | Presented at 43rd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Denver, CO, April 22-25, 2002. | en_US |
| dc.description.abstract | The paper defines an innovative, novel design methodology that results in a product that effectively satisfies the designer's needs and requirements. Use is made of the response surface methodology after consideration of other meta-modeling techniques. Drawbacks of the response surface methodology are mitigated by incorporating sensitivity information in the response surface creation. The definition, application, and eventual implementation of this emerging design tool for new product design is described. The new methodology envisioned will make use of the bi-level integrated system synthesis decomposition for distributed computing. The overall goal is to accomplish cheaper, faster, better designs for structural systems and components. This research leads to the discussion of the use of design tools for structural optimization, including the dynamic aeroelastic constraints. | en_US |
| dc.format.extent | 558717 bytes | |
| dc.format.extent | 1905 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.format.mimetype | text/plain | |
| dc.identifier.uri | http://hdl.handle.net/1853/6257 | |
| dc.language.iso | en_US | en_US |
| dc.publisher | Georgia Institute of Technology | en_US |
| dc.publisher | Georgia Institute of Technology | |
| dc.publisher.original | American Institute of Aeronautics and Astronautics (AIAA) | |
| dc.relation.ispartofseries | ASDL;AIAA-2002-1295 | en_US |
| dc.relation.ispartofseries | ASDL;AIAA-2002-1295 | |
| dc.subject | Aeroelasticity | en_US |
| dc.subject | Bi-level integrated system synthesis | en_US |
| dc.subject | Conceptual design | en_US |
| dc.subject | Design requirements | en_US |
| dc.subject | Design tools | en_US |
| dc.subject | Early phases of design | en_US |
| dc.subject | Metamodeling techniques | en_US |
| dc.subject | Response surface metamodels | en_US |
| dc.subject | Sensitivity coefficients | en_US |
| dc.subject | Structural systems | en_US |
| dc.title | Potential Formulation for Aeroelastic Constraint Analysis in a Conceptual Design Environment | en_US |
| dc.type | Text | |
| dc.type.genre | Paper | |
| dspace.entity.type | Publication | |
| local.contributor.author | Mavris, Dimitri N. | |
| local.contributor.corporatename | Daniel Guggenheim School of Aerospace Engineering | |
| local.contributor.corporatename | Aerospace Systems Design Laboratory (ASDL) | |
| local.contributor.corporatename | College of Engineering | |
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