DGLR-Publikationsdatenbank - Detailansicht
Titel:
Multidisciplinary Wing Analysis and Optimization in the Predesign Phase
Autor(en):
T. Krißler, M. Dugas, N. Kresse
Zusammenfassung:
Two conceptual design tools were used to calculate wing weight and aerodynamic performance within predesign. Both codes have been combined in an automated process chain, exchanging results and using the same set of input data using the optimization software Pointer [12]. Referring to a current technology program, parameter scans and optimization runs of a wing design have been performed. Variations of wing planform, thickness distribution and lift distribution have been investigated. The effect of different objective functions to the optimization process is presented. The importance to include high lift considerations is explained based on the optimization result. Analysis tools to consider these effects in conceptual design are being developed in parallel and will be integrated in the described design process as a next step.
Veranstaltung:
CEAS Conference on Multidisciplinary
Aircraft Design and Optimization; Köln; 2001
Medientyp:
Book Chapter
Sprache:
englisch
Format:
14,8 x 21,0 cm, 10 Seiten
Veröffentlicht:
DGLR-Bericht, 2001, 2001-05, CEAS Conference on Multidisciplinary
Aircraft Design and Optimization; S.155-164; 2001; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Klassifikation:
Stichworte zum Inhalt:
aerodynamics, aircraft design, aeronautics, multidisciplinary design optimisation
Verfügbarkeit:
Bestellbar
Veröffentlicht:
2001
Dieses Dokument ist Teil einer übergeordneten Publikation:
CEAS Conference on Multidisciplinary
Aircraft Design and Optimization