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Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments
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.
| Document Type: | Conference or Workshop Item (Paper) | ||||||
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| Additional Information: | LIDO-Berichtsjahr=2001, | ||||||
| Title: | Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments | ||||||
| Authors: |
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| Date: | 2000 | ||||||
| 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 | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | L - no assignement | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | L ST - Starrflüglertechnologien | ||||||
| DLR - Research theme (Project): | L - Concepts & Integration | ||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik | ||||||
| Deposited By: | Claudia Grant | ||||||
| Deposited On: | 16 Sep 2005 | ||||||
| Last Modified: | 14 Jan 2010 20:21 |
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