1982
DOI: 10.2514/3.44769
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Structural modification to achieve antiresonance in helicopters

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Cited by 10 publications
(4 citation statements)
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“…DSM methods compute the optimal structural modifications (mass, damping and stiffness system parameter modifications) that enable to achieve the desired specifications. Traditionally, structural modification has been widely adopted over the decades to assign natural frequencies [18][19][20], mode shapes [21,22] and antiresonance frequencies [23][24][25]. Recently, DSM has been adopted also to increase the robustness against the system uncertainties in motion planning [26] and to improve the subspace of the allowable motion in linear vibratory feeders excited through harmonic excitation [27].…”
Section: Motivations and State Of The Artmentioning
confidence: 99%
“…DSM methods compute the optimal structural modifications (mass, damping and stiffness system parameter modifications) that enable to achieve the desired specifications. Traditionally, structural modification has been widely adopted over the decades to assign natural frequencies [18][19][20], mode shapes [21,22] and antiresonance frequencies [23][24][25]. Recently, DSM has been adopted also to increase the robustness against the system uncertainties in motion planning [26] and to improve the subspace of the allowable motion in linear vibratory feeders excited through harmonic excitation [27].…”
Section: Motivations and State Of The Artmentioning
confidence: 99%
“…In [88] the application of the antiresonance theory for engineering applications in helicopters is discussed placing either passive, semi-active or active TMDs at collocated or noncollocated locations. In [89] the AA in helicopters is studied in order to absorb the rotor induced vibrations. Two methods are provided: the first one performs AA by modifying only the existing stiffness of two fuselage elements by solving a polynomial.…”
Section: Antiresonance Assignment In Helicoptersmentioning
confidence: 99%
“…Inverse structural modification, on the other hand, is used to identify the changes required to obtain desired dynamic properties, usually expressed in terms of desirable natural frequencies and mode shapes. Several researchers, including Park and Park [2,3], Wang et al [4], Mottershead et al [5], and Kyprianou et al [1,6], have concentrated on the inverse structural modification approach. There are very few studies devoted to the topic of direct structural modification.…”
Section: Introductionmentioning
confidence: 99%