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An Experimental Investigation of Passive Shock/Boundary Layer Interaction Control on an Airfoil: Unsteady Measurements.

Wagner, W. (1997) An Experimental Investigation of Passive Shock/Boundary Layer Interaction Control on an Airfoil: Unsteady Measurements. In: Notes on Numerical Fluid Mechanics Volume 56, EUROSHOCK - Drag Reduction by Passive Control Shock - Results of the Project EUROSHOCK, AER2-CT92-0049 Vieweg. pp. 401-414.

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Document Type:Book Section
Additional Information: LIDO-Berichtsjahr=1997,
Title:An Experimental Investigation of Passive Shock/Boundary Layer Interaction Control on an Airfoil: Unsteady Measurements.
Authors:
AuthorsInstitution or Email of Authors
Wagner, W.UNSPECIFIED
Date:1997
Journal or Publication Title:Notes on Numerical Fluid Mechanics Volume 56, EUROSHOCK - Drag Reduction by Passive Control Shock - Results of the Project EUROSHOCK, AER2-CT92-0049
Refereed publication:Yes
In ISI Web of Science:No
Volume:Volume 56
Page Range:pp. 401-414
Publisher:Vieweg
Status:Published
Keywords:two-dimensional airfoil, control of shock waves, unsteady pressure measurements, boundary layer
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:56

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