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Comparison of Models to Predict Low Engine Order Excitation in a High Pressure Turbine Stage

Jöcker, M. and Kessar, A. and Fransson, T. and Kahl, G. and Rehder, H.-J. (2003) Comparison of Models to Predict Low Engine Order Excitation in a High Pressure Turbine Stage. 10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity in Turbomachines, Durham NC, USA, Sept. 7-11 2003, Durham, NC USA.

Full text not available from this repository.

Abstract

The paper compares three numerical strategies to predict the aerodynamic rotor excitation sources of "Low Engine Order" (LEO) in a high-pressure turbine stage. Main focus is laid on methods to compute the stator exit flow. The aim is to evaluate computationally cheap approaches to avoid modelling the whole circumference of the stator. A single passage viscous strategy, a single passage inviscid linear blade movement strategy and a viscous multi passage sector strategy are compared and evaluated. The assessment of the prediction quality is made by comparison of the computed stator exit flow to experimental data. The main result is that only the global behaviour of the stator exit flow is estimated right, both level and amplitude of Mach number and pressure are computed with poor agreement to experiments. Future evaluations of the resulting rotor excitation pressure are needed to estimate the level of necessary agreement to give acceptable predictions of the low engine order forced response.

Item URL in elib:https://elib.dlr.de/1163/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Comparison of Models to Predict Low Engine Order Excitation in a High Pressure Turbine Stage
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Jöcker, M.KTH StockholmUNSPECIFIED
Kessar, A.KTH StockholmUNSPECIFIED
Fransson, T.KTH StockholmUNSPECIFIED
Kahl, G.MTU MünchenUNSPECIFIED
Rehder, H.-J.UNSPECIFIEDUNSPECIFIED
Date:2003
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Low Engine Order (LEO) excitation, high pressure turbine stage, throat variation, stator exit flow field, comparison of numerical and experimental results, numerical strategies for LEO excitation prediction
Event Title:10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity in Turbomachines, Durham NC, USA, Sept. 7-11 2003
Event Location:Durham, NC USA
Event Type:international Conference
Organizer:Duke University,
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L TT - Triebwerkstechnologien
DLR - Research theme (Project):L - Turbine Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:23

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