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The application of pulse excitation to ground and flight vibration testsA discussion of the relative merits of sinusoidal versus nonharmonic excitation for flight flutter testing is presented. It is concluded that the use of transient excitation is rapidly becoming a necessity. The application of small-scale rocket motors to the excitation of the aircraft is suggested. The design and development of rocket motors specifically for flight flutter testing is described. Methods of measuring and analyzing the transient response of the aircraft are discussed, and the techniques of theoretically predicting the structural response are described.
Document ID
19760003025
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Laidlaw, W. R.
(North American Aviation, Inc. Columbus, OH, United States)
Beals, V. L.
(North American Aviation, Inc. Columbus, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA, Washington Flight Flutter Testing Symp.
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N10113
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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