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Numerical Simulation of a Fully Integrated Engine Ground Test

Keller, Dennis (2016) Numerical Simulation of a Fully Integrated Engine Ground Test. 54th AIAA Aerospace Sciences Meeting, 4-8 Jan 2016, San Diego, Ca, USA.

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In the frame of the DLR project SAMURAI, the German Aerospace Center performed an engine ground test with an installed IAE V2527, which was accompanied by various CFD studies. One of these studies aimed at simulating the experimental set-up, including aircraft, ground and hangar with a RANS approach. Therefore, the two equation eddy viscosity model Menter SST and the Reynolds stress model SSG/LRR-g were utilized. The scope of this paper is to illustrate the numerical approach and results of this simulation. Numerical results from the jet flow were compared with measured data obtained using both a Particle Image Velocimetry and Backward Oriented Schlieren method. Regarding the velocity distributions within the outer jet shear layer, the comparison with particle image velocimetry data showed good agreement especially for the Menter SST turbulence model. However, the turbulent kinetic energy was generally overpredicted in the CFD results.

Item URL in elib:https://elib.dlr.de/108080/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical Simulation of a Fully Integrated Engine Ground Test
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Keller, DennisDennis.Keller (at) dlr.dehttps://orcid.org/0000-0002-1471-9433
Date:January 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Aerodynamics, CFD, Engine Flow Simulation, Reynolds Stress Model
Event Title:54th AIAA Aerospace Sciences Meeting
Event Location:San Diego, Ca, USA
Event Type:international Conference
Event Dates:4-8 Jan 2016
Organizer:American Institute Of Aeronautics And Astronautics
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: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Keller, Dennis
Deposited On:22 Nov 2016 14:59
Last Modified:22 Nov 2016 14:59

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