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Fan Blade Deformation Measurements on the DLR Airbus A320-ATRA by Means of IPCT as Part of the Ground Test Campaign in the Frame of the DLR-project SAMURAI

Kirmse, Tania and Maring, Sandra and Ebel, Paul-Benjamin (2016) Fan Blade Deformation Measurements on the DLR Airbus A320-ATRA by Means of IPCT as Part of the Ground Test Campaign in the Frame of the DLR-project SAMURAI. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing. pp. 629-638. doi: 10.1007/978-3-319-27279-5_55. ISBN 978-3-319-27278-8. ISSN 1612-2909.

Full text not available from this repository.

Official URL: http://www.springer.com/de/book/9783319272788

Abstract

The Image Pattern Correlation Technique (IPCT) was applied to measure the fan blade deformation of the IAE V2527 engine operating at Maximum Continous Thrust (MCT). The ground test on the DLR research aircraft A320-ATRA was a main part of the DLR project SAMURAI which wanted to use the ‘Synergy of Advanced Measurement Techniques for Unsteady and High Reynolds Number Aerodynamic Investigations’. The stereo camera system was fixed in front of the left engine. For certification reasons the correlation pattern had to be projected to the fan by a laser. The IPCT evaluation were improved to cope with the special challenges of the measurement and to enable a comparison with Computational Structural Mechanics (CSM) results finally.

Item URL in elib:https://elib.dlr.de/91240/
Document Type:Contribution to a Collection
Additional Information:Online ISBN: 978-3-642-35680-3, E-ISSN: 1860-0824, DOI: 10.1007/978-3-319-27279-5, Buchuntertitel: Contributions to the 19th STAB/DGLR Symposium Munich, Germany, 2014, Library of Congress Control Number: 2015958857
Title:Fan Blade Deformation Measurements on the DLR Airbus A320-ATRA by Means of IPCT as Part of the Ground Test Campaign in the Frame of the DLR-project SAMURAI
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kirmse, TaniaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Maring, SandraUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ebel, Paul-BenjaminUNSPECIFIEDhttps://orcid.org/0000-0002-7112-7653UNSPECIFIED
Date:2016
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics X
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:132
DOI:10.1007/978-3-319-27279-5_55
Page Range:pp. 629-638
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Dillmann, AndreasDLRUNSPECIFIEDUNSPECIFIED
Heller, GerdAirbus Deutschland, Bremen, GermanyUNSPECIFIEDUNSPECIFIED
Wagner, ClausDLRUNSPECIFIEDUNSPECIFIED
Krämer, EwaldUni Stuttgart, GermanyUNSPECIFIEDUNSPECIFIED
Breitsamter, ChristianTU München, GermanyUNSPECIFIEDUNSPECIFIED
Publisher:Springer International Publishing
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-27278-8
Status:Published
Keywords:IPCT, Fan blade deformation, ground test, engine test
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 (old)
Location: Göttingen , Stuttgart
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Institute of Structures and Design > Design and Manufacture Technologies
Deposited By: Micknaus, Ilka
Deposited On:12 May 2016 15:45
Last Modified:28 Mar 2023 23:42

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