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Titel:

Numerical analyses of a reference wing for combination of hybrid laminar flow control and variable camber

Dokumenttyp:
Zeitschriftenaufsatz
Autor(en):
Jentys, Mauricio M.; Effing, Tim; Breitsamter, Christian; Stumpf, Eike
Abstract:
The objective of the LuFo VI-1 project CATeW (Coupled Aerodynamic Technologies for Aircraft Wings) consists in multifidelity analyses to assess the potential for aerodynamic efficiency increase by combined application of hybrid laminar flow control and variable camber technologies to the wing of a transonic transport aircraft. Individually, both technologies have proven to lead to major aerodynamic drag reductions. An evaluation of the coupled technologies is, therefore, expected to show an even...     »
Stichworte:
Hybrid laminar flow control; Variable camber; Drag reduction
Dewey Dezimalklassifikation:
620 Ingenieurwissenschaften
Zeitschriftentitel:
CEAS Aeronautical Journal
Jahr:
2022
Sprache:
en
Volltext / DOI:
doi:10.1007/s13272-022-00598-y
WWW:
https://link.springer.com/article/10.1007/s13272-022-00598-y
Verlag / Institution:
Springer Science and Business Media LLC
E-ISSN:
1869-55821869-5590
Hinweise:
he funding of the presented investigations within the LuFo VI-1 project CATeW (Coupled Aerodynamic Technologies for Aircraft Wings, FKZ: 20E1917A/B) 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 e.V. (www.gau...     »
Eingereicht (bei Zeitschrift):
12.01.2022
Angenommen (von Zeitschrift):
30.06.2022
Publikationsdatum:
19.07.2022
TUM Einrichtung:
Lehrstuhl für Aerodynamik und Strömungsmechanik
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