Schrauf, G. and Horstmann, K.H. (2000) Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments. CEAS/Drag net European Drag Reduction Conference, Potsdam (de), 19.-21.06.2000.
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Abstract
The e*-method is applied to three large-scale experiments performed in the ONERA S1MA wind tunnel and two flight experiments with the ATTAS VFW614 and a Fokker F100 aircraft. N-factor correlations using incompressible as well compressible linear stability theory obtained for natural and hybrid laminar flow surfaces are discussed.
Item URL in elib: | https://elib.dlr.de/13370/ | |||||||||
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Document Type: | Conference or Workshop Item (Paper) | |||||||||
Additional Information: | LIDO-Berichtsjahr=2001, | |||||||||
Title: | Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments | |||||||||
Authors: |
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Date: | 2000 | |||||||||
Open Access: | No | |||||||||
Gold Open Access: | No | |||||||||
In SCOPUS: | No | |||||||||
In ISI Web of Science: | No | |||||||||
Status: | Published | |||||||||
Keywords: | linear stability theory, two N-factor method, flight tests, wind tunnel tests, natural laminar flow, hybrid laminar flow | |||||||||
Event Title: | CEAS/Drag net European Drag Reduction Conference, Potsdam (de), 19.-21.06.2000 | |||||||||
HGF - Research field: | Aeronautics, Space and Transport (old) | |||||||||
HGF - Program: | Aeronautics | |||||||||
HGF - Program Themes: | other | |||||||||
DLR - Research area: | Aeronautics | |||||||||
DLR - Program: | L ST - Starrflüglertechnologien | |||||||||
DLR - Research theme (Project): | L - Concepts & Integration (old) | |||||||||
Location: | Köln-Porz , Braunschweig , Göttingen | |||||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik | |||||||||
Deposited By: | Grant, Claudia | |||||||||
Deposited On: | 16 Sep 2005 | |||||||||
Last Modified: | 14 Jan 2010 20:21 |
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