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Li, Ding and Hartmann, Ralf (2014) The application of adjoint-based airfoil optimization with discretization error control to a benchmark problem. STAB Symposium 2014, 4-5 Nov. 2014, München, Germany.
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Abstract
Adjoint-based airfoil shape optimization is combined with adaptive mesh refinement and error control.
| Item URL in elib: | https://elib.dlr.de/92447/ | |||||||||
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| Document Type: | Conference or Workshop Item (Speech) | |||||||||
| Title: | The application of adjoint-based airfoil optimization with discretization error control to a benchmark problem | |||||||||
| Authors: |
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| Date: | 5 November 2014 | |||||||||
| Refereed publication: | Yes | |||||||||
| Open Access: | No | |||||||||
| Gold Open Access: | No | |||||||||
| In SCOPUS: | No | |||||||||
| In ISI Web of Science: | No | |||||||||
| Status: | Published | |||||||||
| Keywords: | shape optimization, adaptive mesh refinement, error estimation | |||||||||
| Event Title: | STAB Symposium 2014 | |||||||||
| Event Location: | München, Germany | |||||||||
| Event Type: | national Conference | |||||||||
| Event Dates: | 4-5 Nov. 2014 | |||||||||
| HGF - Research field: | Aeronautics, Space and Transport | |||||||||
| HGF - Program: | Aeronautics | |||||||||
| HGF - Program Themes: | fixed-wing aircraft | |||||||||
| DLR - Research area: | Aeronautics | |||||||||
| DLR - Program: | L AR - Aircraft Research | |||||||||
| DLR - Research theme (Project): | L - Simulation and Validation (old) | |||||||||
| Location: | Braunschweig | |||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering | |||||||||
| Deposited By: | Hartmann, Dr.rer.nat. Ralf | |||||||||
| Deposited On: | 25 Nov 2014 09:42 | |||||||||
| Last Modified: | 29 Mar 2023 00:21 |
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