Numerical and experimental investigation of the design of a piezoelectric de-icing system for small rotorcraft part 2/3: investigation of transient vibration during frequency sweeps and optimal piezoelectric actuator excitation

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DOIResolve DOI: https://doi.org/10.3390/aerospace7050049
AuthorSearch for: ORCID identifier: https://orcid.org/0000-0003-2083-3758; Search for: ; Search for: 1
Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Subjecticing; rotorcraft; ice protection system; piezoelectric actuator; vibration; numerical model; experimental testing
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PublisherMDPI
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LanguageEnglish
Peer reviewedYes
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Record identifier942189f9-8910-4243-b471-a4b62b9b00c0
Record created2020-06-19
Record modified2020-06-23
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