DGLR-Publikationsdatenbank - Detailansicht
Titel:
EPISTLE: High Lift System Design for Low-Noise Applied to a Supersonic Aircraft
Autor(en):
U. Herrmann
Zusammenfassung:
A new approach for low-drag high-lift system design based on the application of viscous flow solvers is developed by the EC research project EPISTLE. Two highlift systems for Supersonic Commercial Transport (SCT) wings are designed and manufactured as a wind tunnel model. The large numerically predicted drag reductions are fully confirmed by high Reynolds number tests. These drag reductions significantly lower the low-speed noise of future SCT configurations.
Veranstaltung:
CEAS/KATnet Conference on Key Aerodynamic Technologies, Bremen, 2005
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 8 Seiten
Veröffentlicht:
DGLR-Bericht, 2005, 2005-07, CEAS/KATnet Conference on Key Aerodynamic Technologies - Proceedings; S.1-8; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
in getr. Zählung;
Klassifikation:
Stichworte zum Inhalt:
aerodynamics
Verfügbarkeit:
Bibliothek
Veröffentlicht:
2005
Dieses Dokument ist Teil einer übergeordneten Publikation:
CEAS/KATnet Conference on Key Aerodynamic Technologies - Proceedings