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Simulation Quality Optimization of a Turbofan Simulator by Means of a 3D Navier-Stokes Method

Bolms, H.-Th. (1996) Simulation Quality Optimization of a Turbofan Simulator by Means of a 3D Navier-Stokes Method. Engine-Airframe Integration Conference, The Royal Aeronautical Society, 10.-11. Oktober 1996, Bristol.

Full text not available from this repository.

Abstract

With a 3D-Navier-Stokes code differences between the isolated, axisymmetrical flow fields of an actual engine and its TPS are calculated. The influence of the turbine jet on the external flow is shown. Recommendations for the main simulation parameters are given. The potential for improvements of the TPS-technique is described. A TPS with an optimized flow-field simulation quality is presented.

Item URL in elib:https://elib.dlr.de/37519/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Simulation Quality Optimization of a Turbofan Simulator by Means of a 3D Navier-Stokes Method
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Bolms, H.-Th.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1996
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Engine simulation, quality of simulation, 3D Navier-Stokes code
Event Title:Engine-Airframe Integration Conference, The Royal Aeronautical Society, 10.-11. Oktober 1996, Bristol
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:08

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