Numerical and experimental investigation of a single-axis parallel active vibration mount for helicopter seats using vibration standards

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/1.4046383
AuthorSearch for: 1; Search for: 1; Search for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Physical description13 p.
Subjectactuators; control equipment; filters; vibration; simulation; elastomers; vibration control; computer simulation
Abstract
Publication date
PublisherAmerican Society of Mechanical Engineers
In
LanguageEnglish
Peer reviewedYes
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Record identifier528a5e8a-0f29-4e9d-a760-acc5384eed38
Record created2022-05-16
Record modified2022-05-16
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