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Integrated Design Method for Aircraft with Hybrid Laminar Flow Control Wings

Risse, Kristof and Stumpf, Eike (2016) Integrated Design Method for Aircraft with Hybrid Laminar Flow Control Wings. 7th European Congress on Computational Methods in Applied Sciences and Engineering 2016, 2016-06-05 - 2016-06-10, Hersonissos, Griechenland.

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Item URL in elib:https://elib.dlr.de/109879/
Document Type:Conference or Workshop Item (Speech)
Title:Integrated Design Method for Aircraft with Hybrid Laminar Flow Control Wings
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Risse, KristofUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Stumpf, EikeUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:June 2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Overall Aircraft Design, Wing Design, Hybrid Laminar Flow Control, HLFC
Event Title:7th European Congress on Computational Methods in Applied Sciences and Engineering 2016
Event Location:Hersonissos, Griechenland
Event Type:international Conference
Event Start Date:5 June 2016
Event End Date:10 June 2016
Organizer:European Community on Computational Methods in Applied Sciences (ECCOMAS)
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 - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Risse, Kristof
Deposited On:20 Dec 2016 13:37
Last Modified:24 Apr 2024 20:15

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