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.
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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/ | ||||||||||||||||||||||||
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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: |
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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: |
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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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