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Application of antiresonance theory to helicoptersAntiresonance theory is the principle underlying nonresonant nodes in a structure, and covers both nonresonant nodes occurring naturally and those introduced by devices such as dynamic absorbers and antiresonant isolators. The dynamic antiresonant vibration isolator (DAVI) and the nodale module are examples of the applications of transfer antiresonances. It is shown that antiresonances are eigenvalues, and that they can be determined by matrix iteration. Applications of antiresonance theory to helicopter engineering problems, using the antiresonant eigenvalue equation are suggested.
Document ID
19740026386
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bartlett, F. D., Jr.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Flannelly, W. G.
(Kaman Aerospace Corp. Bloomfield, CT, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Publication Information
Publication: NASA. Ames Res. Center Rotorcraft Dyn.
Subject Category
Structural Mechanics
Accession Number
74N34499
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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