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.

Item URL in elib:

https://elib.dlr.de/13370/

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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Schrauf, G.	EADS	UNSPECIFIED	UNSPECIFIED
Horstmann, K.H.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2000

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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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