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Hazra, Subhendu und Schulz, Volker und Brezillon, Joel (2008) Simultaneous Pseudo-Time Stepping for 3D Aerodynamic Shape Optimization. Numerical Mathematics, 16 (Heft 2), Seiten 139-161. Walter de Gruyter . doi: 10.1515/JNUM.2008.007.
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Kurzfassung
This paper presents a numerical method for aerodynamic shape optimization problems with state constraint. It uses a simultaneous semi-iterative technique to solve the equations arising from the first order necessary optimality conditions. The method converges without additional globalization in the design space. A reduced SQP method based preconditioner is used for convergence acceleration. Design examples of drag reduction with constant lift for wing and body of a Supersonic Commercial Transport (SCT) aircraft are included. The overall cost of computation is about 8 forward simlation runs.
| elib-URL des Eintrags: | https://elib.dlr.de/21240/ | ||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||
| Titel: | Simultaneous Pseudo-Time Stepping for 3D Aerodynamic Shape Optimization | ||||||||||||||||
| Autoren: |
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| Datum: | Juni 2008 | ||||||||||||||||
| Erschienen in: | Numerical Mathematics | ||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||
| Open Access: | Ja | ||||||||||||||||
| Gold Open Access: | Ja | ||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||
| Band: | 16 | ||||||||||||||||
| DOI: | 10.1515/JNUM.2008.007 | ||||||||||||||||
| Seitenbereich: | Seiten 139-161 | ||||||||||||||||
| Verlag: | Walter de Gruyter | ||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||
| Stichwörter: | shape optimization, simultaneous pseudo-time stepping, Euler equations, preconditioner, reduced SQP methods, supersonic aircraft. | ||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||
| HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||
| DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation & Validierung (alt) | ||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > CASE | ||||||||||||||||
| Hinterlegt von: | Brezillon, Joel | ||||||||||||||||
| Hinterlegt am: | 25 Nov 2010 09:31 | ||||||||||||||||
| Letzte Änderung: | 24 Apr 2024 19:02 |
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