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Shake Tests on the EC 135 Helicopter.

Degener, M. (1994) Shake Tests on the EC 135 Helicopter. DLR-Interner Bericht. 232 - 94 C 17, 81 S.

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Abstract

Shake tests were performed on the new multi-purpose helicopter EC 135 developed by Eurocopter. The purpose of the tests was the evaluation of the performance characteristics of the installed vibration reduction system ARIS. Comprehensive investigations on the tuning capabilities of the system were performed. Furthermore, significant normal modes were identified to enable a correlation with the mathematical predictions. The present report describes the test performance and summarizes the main test results.

Item URL in elib:https://elib.dlr.de/39684/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Shake Tests on the EC 135 Helicopter.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Degener, M.UNSPECIFIEDUNSPECIFIED
Date:1994
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:81
Status:Published
Keywords:Helicopter, vibrations, shake test, vibration reduction, EC 135.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L SI - Versuchs- und Simulationstechniken
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 10:51

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