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Normal Mode Testing by Multi-Axial Base Excitation.

Sinapius, M. (1997) Normal Mode Testing by Multi-Axial Base Excitation. In: International Forum on Aeroelasticity and Structural Dynamics, 1997, Volume III, Seiten 209-214. CEAS - International Conference on Aeroelasticity and Structural 17-20 June, 1997, Rome, Italy.

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Kurzfassung

Normal mode testing is commonly performed by multiple point excita- tion. For each normal mode the exciter configuration is adapted in location and magnitude in order to compensate for the internal damping forces of the test structure. An alternative to multiple point excitation is a driven-base test using a multi-axial shaker table. Multi-axis shaker facilities have been developed for structural dynamic qualification. However, they can be used for normal mode testing as well. Then, the overall structure is accelerated in space in order to compensate for the internal damping forces. This requires a suitable combination of all six spatial degrees of freedom of the base excitation. In the case of resonance, the structure responds in quadrature related to the base excitation. If this criterion is fulfilled, the structure vibrates in an eigenmode of vibration in the sense of a single degree of freedom system. The paper summarizes the theoretical background of the test method with particular emphasis on the damping estimation, on the determination of the generalized mass, and on finding a suitanble base axis combination. A suitable test rig for the normal mode testing by base excitation, DLR's multi- axis vibration simualtor MAVIS in Goettingen (FRG) is presented. The test procedure and test data evaluation are elucidated. The application on a test structure characterized by closely-spaced eigenfrequencies is presented. The advantages and disadvantages of normal mode testing by means of base excitation are pointed out.

elib-URL des Eintrags:https://elib.dlr.de/39816/
Dokumentart:Konferenzbeitrag (Paper)
Zusätzliche Informationen: LIDO-Berichtsjahr=1997,
Titel:Normal Mode Testing by Multi-Axial Base Excitation.
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Sinapius, M.NICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:1997
Erschienen in:International Forum on Aeroelasticity and Structural Dynamics, 1997, Volume III
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Seitenbereich:Seiten 209-214
Name der Reihe:Volume II
Status:veröffentlicht
Stichwörter:experimental modal analysis, multi-axial base excitation, normal mode testing
Veranstaltungstitel:CEAS - International Conference on Aeroelasticity and Structural 17-20 June, 1997, Rome, Italy
HGF - Forschungsbereich:NICHT SPEZIFIZIERT
HGF - Programm:Weltraum (alt)
HGF - Programmthema:W RP - Raumtransport
DLR - Schwerpunkt:NICHT SPEZIFIZIERT
DLR - Forschungsgebiet:W RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):NICHT SPEZIFIZIERT
Standort: Göttingen
Institute & Einrichtungen:Institut für Aeroelastik
Hinterlegt von: DLR-Beauftragter, elib
Hinterlegt am:02 Apr 2006
Letzte Änderung:27 Apr 2009 10:55

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