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Flow field investigations in the free bypass jet flow of a V2527 engine at Ground Operation using SPIV

Schröder, Andreas and Geisler, Reinhard and Schanz, Daniel and Wrede, Björn and Agocs, Janos (2016) Flow field investigations in the free bypass jet flow of a V2527 engine at Ground Operation using SPIV. AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting, 04. - 08. Jan. 2016, San Diego, CA, USA. DOI: 10.2514/6.2016-0108

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0108

Abstract

The investigation of the flow field at the nozzle exit of a full scale aero-engine using Stereo Particle Image Velocimetry (SPIV) aims at providing important reference and validation data required for reliable modeling and prediction. Furthermore, the turbulent jet engine exhaust flow is of prominent interest for the aerodynamic and -acoustic characterization of an aircraft engine. Especially the development of the free shear-layer between fan-bypass flow and outer flow is an important source of high-frequency noise as well as of big interest for modeling the turbulence of a jet flow correctly by advanced RANS methods. The SPIV measurements have been performed at free running fan phase positions and with a large number of statistically independent samples enabling a turbulence characterization of the fan-bypass and corresponding shear layer flow based on mean- and RMS-fields of all three velocity components, POD analysis and two-point-correlation functions.

Item URL in elib:https://elib.dlr.de/100709/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA-2016-0108
Title:Flow field investigations in the free bypass jet flow of a V2527 engine at Ground Operation using SPIV
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schröder, Andreasandreas.schroeder (at) dlr.deUNSPECIFIED
Geisler, Reinhardreinhard.geisler (at) dlr.deUNSPECIFIED
Schanz, Danieldaniel.schanz (at) dlr.deUNSPECIFIED
Wrede, Björnbjoern.wrede (at) dlr.deUNSPECIFIED
Agocs, Janosjanos.agocs (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2016-0108
Page Range:pp. 1-14
Series Name:Conference Proceedings online
Status:Published
Keywords:SPIV, velocity fields, aircraft engine, MCT, POD, two-point-correlation
Event Title:AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting
Event Location:San Diego, CA, USA
Event Type:international Conference
Event Dates:04. - 08. Jan. 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:18 May 2016 09:59
Last Modified:18 May 2016 09:59

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