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Ground Vibration Tests on the Aircraft PC-12.

Degener, M. (1991) Ground Vibration Tests on the Aircraft PC-12. DLR-Interner Bericht. 232-91 C 06. 125 S.

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To meet the FAA flutter certification requirements of the Federal Aviation Requirements Part 23, ground vibration tests were performed on the prototype of the PC-12 aircraft. The tests were performed with the mobile ground vibration test facility of DLR under contract of Pilatus Aircraft Ltd. in Stans (Switzerland). The aircraft was investigated in five configurations. For all normal modes the modal parameters were measured and checked for their linearity behavior. The test results are presented in this report.

Item URL in elib:https://elib.dlr.de/39425/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1991,
Title:Ground Vibration Tests on the Aircraft PC-12.
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Open Access:No
Number of Pages:125
Keywords:Flutter, Ground Vibration Test, Modal analysis.
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
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 10:42

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