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Ground Vibration Tests on the Airbus A321 Aircraft Equipped with IAE V2530-A5 Engines.

Degener, M. and Füllekrug, U. and Sinapius, M. (1993) Ground Vibration Tests on the Airbus A321 Aircraft Equipped with IAE V2530-A5 Engines. DLR-Interner Bericht. 232-93 C 02, 283 S.

Full text not available from this repository.

Abstract

This report describes the ground vibration tests performed on the first prototype of the Airbus A321 aircraft equipped with IAE V2530-A5 engines. The extensive test program included the aircraft with empty and full tanks, failure cases, extended landing flaps, and landing gear. In all configurations the normal mode parameters were measured including linearity tests. All test results are summarized in this report. The respective tests performed on the second prototype equipped with CFM56-5B engines are described in a separate report.

Item URL in elib:https://elib.dlr.de/39605/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1993,
Title:Ground Vibration Tests on the Airbus A321 Aircraft Equipped with IAE V2530-A5 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:283
Status:Published
Keywords:Ground Vibration Test, Normal Modes, 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 10:48

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