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Titel:

TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Jentys, Mauricio M.; Breitsamter, Christian
Abstract:
This paper presents computational fluid dynamics (CFD) results of the transitional flow field around a transonic transport aircraft wing. The framework for the analyses is formed by the german LuFo VI-1 project CATeW (Coupled Aerodynamic Technologies for Aircraft Wings), where benefits of the technology coupling between a hybrid laminar flow control (HLFC) system and a variable camber (VC) wing on aerodynamic drag is assessed. The computational fluid dynamics framework for the modelling of both...     »
Stichworte:
CFD; Drag Reduction; Hybrid Laminar Flow Control; Transition Prediction; Variable Camber
Dewey-Dezimalklassifikation:
620 Ingenieurwissenschaften
Kongress- / Buchtitel:
33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022
Band / Teilband / Volume:
4
Datum der Konferenz:
4 September 2022through 9 September 2022
Verlag / Institution:
International Council of the Aeronautical Sciences
Jahr:
2022
Seiten:
2961 – 2976
Nachgewiesen in:
Scopus
Print-ISBN:
978-171387116-3
Sprache:
en
WWW:
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85159581120&partnerID=40&md5=22a0b1efd758e4cd8deeaa0a1c14049e
Hinweise:
Funding text The funding of the presented investigations within the LuFo VI-1 project CATeW (Coupled Aerodynamic Technologies for Aircraft Wings, FKZ: 20E1917B) by the German Federal Ministry for Economic Affairs and Climate Action (BMWK) is gratefully acknowledged. Furthermore, the authors deeply appreciate the German Aerospace Center (DLR) for providing the DLR TAU Code used for the numerical HiFi - investigations. Moreover, the authors would like to thank the Gauss Centre for Supercomputing...     »
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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