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Ground vibration test results of a JetStar airplane using impulsive sine excitationStructural excitation is important for both ground vibration and flight flutter testing. The structural responses caused by this excitation are analyzed to determine frequency, damping, and mode shape information. Many excitation waveforms have been used throughout the years. The use of impulsive sine (sin omega t)/omega t as an excitation waveform for ground vibration testing and the advantages of using this waveform for flight flutter testing are discussed. The ground vibration test results of a modified JetStar airplane using impulsive sine as an excitation waveform are compared with the test results of the same airplane using multiple-input random excitation. The results indicated that the structure was sufficiently excited using the impulsive sine waveform. Comparisons of input force spectrums, mode shape plots, and frequency and damping values for the two methods of excitation are presented.
Document ID
19900029908
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kehoe, Michael W.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Voracek, David F.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: International Modal Analysis Conference
Location: Las Vegas, NV
Country: United States
Start Date: January 30, 1989
End Date: February 2, 1989
Sponsors: Union College, SEM
Accession Number
90A16963
Distribution Limits
Public
Copyright
Other

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