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Dynamic Stall Investigations on the Pitching DSA-9A Rotor Blade Tip Model in the SWG – Test Campaign 2014

Merz, Christoph B. (2016) Dynamic Stall Investigations on the Pitching DSA-9A Rotor Blade Tip Model in the SWG – Test Campaign 2014. DLR-Interner Bericht. DLR-IB 224-2015 A 115, 70 S.

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Abstract

Measurement report of the first STELAR pitching rotor blade tip experiment in the low speed wind tunnel SWG, including an overview of the data processing and references to published data of this experiment.

Item URL in elib:https://elib.dlr.de/102925/
Document Type:Monograph (DLR-Interner Bericht)
Title:Dynamic Stall Investigations on the Pitching DSA-9A Rotor Blade Tip Model in the SWG – Test Campaign 2014
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Merz, Christoph B.christoph.merz (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:70
Status:Published
Keywords:Dynamic Stall, Wind tunnel experiments, PIV
Institution:DLR
Department:AS-HEL
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: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Helicopter, GO
Deposited By: Bachmann, Barbara
Deposited On:25 Jan 2017 15:10
Last Modified:24 Aug 2018 09:23

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