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Time-Linearized Forced Response Analysis of a Counter Rotating Fan; Part I: Theoretical Concept of a Fully Time-Linear Forced Response Analysis

Blocher, Michael and Gómez Fernández, Io Eunice (2014) Time-Linearized Forced Response Analysis of a Counter Rotating Fan; Part I: Theoretical Concept of a Fully Time-Linear Forced Response Analysis. In: ASME Turbo Expo. ASME Turbo Expo 2014, 16-20 Jun 2014, Düsseldorf, Germany.

Full text not available from this repository.

Abstract

From 2010 to 2013, several institutes of the German Aerospace Center investigated a counter rotating fan arrangement called CRISP2. While having efficiency advantages over rotor-stator arrangements, counter rotating fans might be subject to increased aerodynamic excitation as well. It is well known that rotor-stator interaction (in this case rotor-rotor-interaction) can result in aerodynamic excitation of blades leading to high cycle fatigue. Therefore, forced response calculations and an estimation of the static and dynamic loads during operation are essential prior to production and rig tests. At the Institute of Aeroelasticity, loosely coupled approaches for forced response calculations have been employed for a number of years (VASANTHAKUMAR [1]). Due to a limited time frame for the forced response simulation, it was decided to use this loosely coupled approach for the forced response simulations in CRISP2 as well and to reduce its time consumption even more by using a time-linear approach for the forcing calculations. The theoretical concepts and their implementation into a forced response simulation are highlighted. Special consideration is given to the linearized unsteady simulations with gust boundary conditions that have been implemented into the DLR in-house flow solver TRACE [2]. The advantages and drawbacks of a fully time-linear loosely coupled method compared to more accurate and complicated approaches are discussed.

Item URL in elib:https://elib.dlr.de/91078/
Document Type:Conference or Workshop Item (Speech)
Title:Time-Linearized Forced Response Analysis of a Counter Rotating Fan; Part I: Theoretical Concept of a Fully Time-Linear Forced Response Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Blocher, Michaelmichael.blocher (at) dlr.deUNSPECIFIED
Gómez Fernández, Io EuniceAE-EXTUNSPECIFIED
Date:June 2014
Journal or Publication Title:ASME Turbo Expo
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Status:Published
Keywords:aeroelasticity, forced response, turbomachines, time-linear, energy method
Event Title:ASME Turbo Expo 2014
Event Location:Düsseldorf, Germany
Event Type:international Conference
Event Dates:16-20 Jun 2014
Organizer:ASME IGTI
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Blocher, Michael
Deposited On:14 Nov 2014 15:43
Last Modified:09 Feb 2017 19:20

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