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Cost-effective HLFC design concept for transport aircraft

Horn, Matthias and Seitz, Arne and Schneider, Marvin (2019) Cost-effective HLFC design concept for transport aircraft. In: DGLR BERICHTE. Deutscher Luft- und Raumfahrtkongress 2019, 30.09. - 02.10.2019, Darmstadt, Deutschland. DOI: 10.25967/490059

Full text not available from this repository.

Official URL: https://doi.org/10.25967/490059

Abstract

Resource-efficient flying is a central goal of current and future developments in aviation. Laminar technology is one of the most promising ways to contribute for the achievements to reach the goals of Flightpath 2050. The hybrid laminar flow control (HLFC), based on the combination of active flow control by boundary layer suction and natural laminar flow downstream, is a favourable way to laminarize leading edges with large sweep angle. While the resistance-reducing effective of HLFC technology has already been proven with wind tunnel and flight tests, solutions for the cost-effective production are still subject of current developments. The particular difficulty lies in the combination of industrially producible designs while maintaining the aerodynamic performance. For this purpose, DLR is developing a leading-edge design, based on a cost-effective, micro-perforated outer skin with intrinsic pressure drop distribution. Furthermore the leading edge will be fully demountable for maintenance and cleaning reasons. The resulting combination of low manufacturing and operational costs should leverage the breakthrough of HLFC technology for industrial application. In the following paper the aerodynamic and structural design of the leading edge as well as the manufacturing technology of the outer skin are described. In addition the structural concept for fin application is presented. The presented work and achieved results were developed in the CleanSky2 project NACOR (New Aircraft Configurations and Related Issues, Grant Agreement No. CS2-AIR-GAM-2014-2015-01), funded by the European Commission and the Federal Ministry for Economic Affairs and Energy.

Item URL in elib:https://elib.dlr.de/130623/
Document Type:Conference or Workshop Item (Speech)
Title:Cost-effective HLFC design concept for transport aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Horn, MatthiasMatthias.Horn (at) dlr.dehttps://orcid.org/0000-0001-5092-2415
Seitz, ArneArne.Seitz (at) dlr.deUNSPECIFIED
Schneider, MarvinMarvin.Schneider (at) dlr.dehttps://orcid.org/0000-0002-4110-8443
Date:14 November 2019
Journal or Publication Title:DGLR BERICHTE
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
DOI :10.25967/490059
Status:Published
Keywords:HLFC, laminar, active flow control
Event Title:Deutscher Luft- und Raumfahrtkongress 2019
Event Location:Darmstadt, Deutschland
Event Type:national Conference
Event Dates:30.09. - 02.10.2019
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures and Materials
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Design and Manufacture Technologies
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Horn, Matthias
Deposited On:19 Nov 2019 12:06
Last Modified:19 Nov 2019 12:06

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