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Experimental Investigation of the Flowfield around a Multielement Airfoil.

Nakayama, A. (1) and Kreplin, H.-P. and Morgan, H. L. (2) (1990) Experimental Investigation of the Flowfield around a Multielement Airfoil. AIAA Journal 28 (1990) No. 1, pp. 14-21.

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Detailed measurements on mean flow and turbulence around a multielement airfoil model have been made using pressure and hot-wire probes. The results obtained in two test cases at chord Reynolds number of 3 x 10 exponent 6 and freestream Mach number of 0.2 show a number of features of the complex flows that are important for accurately modeling these flows by numerical methods. Many parts of the shear flow deviated vastly from classical flows, and the interaction with the external flow is very strong.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=1990, note=834, pages=8,
Title:Experimental Investigation of the Flowfield around a Multielement Airfoil.
AuthorsInstitution or Email of Authors
Nakayama, A. (1)UNSPECIFIED
Morgan, H. L. (2)UNSPECIFIED
Journal or Publication Title:AIAA Journal 28 (1990) No. 1
Refereed publication:Yes
In ISI Web of Science:Yes
Page Range:pp. 14-21
Keywords:Hochautriebssystem, Grenzschicht, Nachlauf, Turbulenz
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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