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Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data

Gardner, Anthony Donald and Richter, Kai (2014) Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data. 19. DGLR-Fachsymposium der STAB, 04. – 05. Nov. 2014, München, Deutschland.

Full text not available from this repository.

Official URL: http://www.stab2014.tum.de/

Abstract

This paper will show a method of measuring the transition position for a periodically pitching airfoil using the unsteady pressure transducers which are required to measure the airfoil loads in the experiment.

Item URL in elib:https://elib.dlr.de/89547/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Die positiv begutachteten Beiträge werden in der Springer-Reihe „Notes on Numerical Fluid Mechanics and Multidisciplinary Design“ veröffentlicht.
Title:Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gardner, Anthony Donaldtony.gardner (at) dlr.deUNSPECIFIED
Richter, Kaikai.richter (at) dlr.deUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 102-103
Series Name:Jahresbericht 2014
Status:Published
Keywords:periodic pitching airfoil, Helicopter rotor blades, turbulence frequencies
Event Title:19. DGLR-Fachsymposium der STAB
Event Location:München, Deutschland
Event Type:national Conference
Event Dates:04. – 05. Nov. 2014
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 of Aerodynamics and Flow Technology > Helicopters
Deposited By: Micknaus, Ilka
Deposited On:12 Nov 2014 13:19
Last Modified:12 Nov 2014 13:19

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