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Ground Vibration Tests on the Airbus A321 Aircraft Equipped with CFM56-5B Engines.

Degener, M. and Füllekrug, U. and Sinapius, M. (1993) Ground Vibration Tests on the Airbus A321 Aircraft Equipped with CFM56-5B Engines. DLR-Interner Bericht. 232-93 C 10, 167 S.

Full text not available from this repository.

Abstract

This report describes the ground vibration tests performed on the second prototype of the Airbus A321 aircraft equipped with CFM56-5B engines. The tests were carried out at the final assembly line in Hamburg during March, 1993. The investigations were performed on the aircraft with empty fuel tanks. Up to 50 Hz the normal mode parameters were measured including linearity checks. All test results are summarized in this report. The respective tests performed on the first aircraft prototype equipped with IAE V2530-A5 engines are described in a separate report.

Item URL in elib:https://elib.dlr.de/39618/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1993,
Title:Ground Vibration Tests on the Airbus A321 Aircraft Equipped with CFM56-5B Engines.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Degener, M.UNSPECIFIEDUNSPECIFIED
Füllekrug, U.UNSPECIFIEDUNSPECIFIED
Sinapius, M.UNSPECIFIEDUNSPECIFIED
Date:1993
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:167
Status:Published
Keywords:Airbus, Ground Vibration Test, Flutter.
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: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:49

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