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Aerodynamic Experimental Results from the Hybrid Laminar Flow Nacelle Flight Demonstration on the VFW614/ATTAS Aircraft

Riedel, H. and Sitzmann, M. and Petersik, M. (2016) Aerodynamic Experimental Results from the Hybrid Laminar Flow Nacelle Flight Demonstration on the VFW614/ATTAS Aircraft. DLR-Interner Bericht. DLR-IB-AS-BS-2016-11, 2657 S.

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Item URL in elib:https://elib.dlr.de/116680/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information:IB auf CD
Title:Aerodynamic Experimental Results from the Hybrid Laminar Flow Nacelle Flight Demonstration on the VFW614/ATTAS Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Riedel, H.hansgeorg.riedel (at) dlr.deUNSPECIFIED
Sitzmann, M.martin.sitzmann (at) dlr.deUNSPECIFIED
Petersik, M.UNSPECIFIEDUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:2657
Status:Published
Keywords:Hybrid Laminar Flow Nacelle, Flight Tests, Transport Aircraft, Aerodynamic Results, Accuracy Estimate of some Key Flight and Aerodynamic Parameters
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
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Seyfried, Beate
Deposited On:07 Dec 2017 15:48
Last Modified:07 Dec 2017 15:48

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