Aerodynamic drag reduction through a hybrid laminar flow control and variable camber coupled wing

Title:: Aerodynamic drag reduction through a hybrid laminar flow control and variable camber coupled wing
Document type:: Zeitschriftenaufsatz
Author(s):: Jentys, Mauricio; Breitsamter, Christian
Dewey Decimal Classification:: 620 Ingenieurwissenschaften
Journal title:: Aerospace Science and Technology
Year:: 2023
Journal volume:: 142
Pages contribution:: 108652
Covered by:: Scopus
Language:: en
Fulltext / DOI:: doi:10.1016/j.ast.2023.108652
Publisher:: Elsevier BV
E-ISSN:: 1270-9638
Notes:: 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 e.V.
Date of publication:: 01.11.2023
TUM Institution:: Lehrstuhl für Aerodynamik und Strömungsmechanik
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