elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

lnfluence of a back-flow flap on the dynamic stall flow topology

Wolf, Christian C. and Gardner, Anthony and Merz, Christoph B. and Opitz, Steffen (2018) lnfluence of a back-flow flap on the dynamic stall flow topology. CEAS Aeronautical Journal, 9 (39), pp. 39-51. Springer. DOI: 10.1007/s13272-017-0274-z ISSN 1869-5590

[img] PDF
3MB

Official URL: https://link.springer.com/article/10.1007/s13272-017-0274-z

Abstract

Dynamic stall is a major concern for highly loaded helicopter rotors in fast forward flight. The potential of a backflow flap for dynamic stall reduction is investigated. The flap assembly is mounted on the suction side of a helicopter airfoil undergoing deep-stall pitch oscillations. Wind-tu nnel experiments using high-speed particle image velocimetry were conducted to identify the flow topology and to imiestigate the flap's method of operation. A phaseaveraged proper orthogonal decomposition (POD) is used to identify relevant flow events and to compare test cases with and without flap. The evolution of the la rge-scale dynamic stall vortex in the in itial phases of flow separation is analyzed in detail. The back-flow flap splits the vortex into two smaller vortices and thereby reduces the pitching moment peak. This effect can be described through the eigenmode coefficients of the POD. The study closes with an analysis of different pitching frequencies, which do not affect the flap's method of operation.

Item URL in elib:https://elib.dlr.de/111117/
Document Type:Article
Additional Information:First online: 13. November 2017; Online ISSN: 1869-5590; Druckversion erschienen: März 2018; Print ISSN: 1869-5582
Title:lnfluence of a back-flow flap on the dynamic stall flow topology
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wolf, Christian C.christian.wolf (at) dlr.deUNSPECIFIED
Gardner, Anthonyanthony.gardner (at) dlr.dehttps://orcid.org/0000-0002-1176-3447
Merz, Christoph B.Daimler AGUNSPECIFIED
Opitz, Steffensteffen.opitz (at) dlr.deUNSPECIFIED
Date:2018
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:9
DOI :10.1007/s13272-017-0274-z
Page Range:pp. 39-51
Publisher:Springer
Series Name:Springer Nature
ISSN:1869-5590
Status:Published
Keywords:Helicopter rotor, Wind tunnel, Flow control, Dynamic stall, Experiment
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Helicopter, GO
Institute of Composite Structures and Adaptive Systems > Multifunctional Materials
Deposited By: Bachmann, Barbara
Deposited On:17 Nov 2017 11:04
Last Modified:31 Jul 2019 20:08

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.