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Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections

Wild, Jochen (2013) Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections. Journal of Aircraft, 50 (4), pp. 1202-1216. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C032138 ISSN 0021-8669

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/abs/10.2514/1.C032138

Abstract

Experimental investigations have been carried out with the two-dimensional DLR-F15 high-lift wing-section model in the Cryogenic Wind-tunnel Cologne DNW-KKK to differentiate between the influence of Mach and Reynolds numbers on the stall behavior. Because of the cryogenic environment, Mach and Reynolds numbers have been varied independently between M=0.1–0.25 and Re=1.4×10^6 − 15.6×10^6. The investigation covers two- and three element configurations at various slat and flap settings and two different slat shapes. The focus of the investigation is to identify conditions of turbulent leading-edge stall, shock-related lift limitations, and flap separations and their influence on achievable maximum lift coefficient.

Item URL in elib:https://elib.dlr.de/87409/
Document Type:Article
Title:Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:July 2013
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:50
DOI :10.2514/1.C032138
Page Range:pp. 1202-1216
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:aerodynamics, high-lift, stall
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Wild, Dr.-Ing. Jochen
Deposited On:10 Jan 2014 09:45
Last Modified:08 Mar 2018 18:41

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