NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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
19890006538
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kehoe, Michael W.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Voracek, David F.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-100448
H-1504
NAS 1.15:100448
Report Number: NASA-TM-100448
Report Number: H-1504
Report Number: NAS 1.15:100448
Meeting Information
Meeting: International Modal Analysis Conference
Location: Las Vegas, NV
Country: United States
Start Date: January 30, 1989
End Date: February 2, 1989
Accession Number
89N15909
Funding Number(s)
PROJECT: RTOP 505-63-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available