Enhancement of ultrasonic De-icing via transient excitation

Nicola DiPlacido, Jared Soltis, Edward Smith, Jose Palacios

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Abstract

Previous ultrasonic de-icing research on rotorcraft has shown that a multi-frequency tone burst actuation scheme has increased the coverage of the deicing system. The physical mechanisms responsible for this increase in de-icing performance are modeled using finite elements and tested using both freezer ice on a titanium plate and impact ice under rotation in the AERTS facility on a NACA 0015 airfoil structure. Burst actuation techniques are shown to have up to 400% increase in de-icing potential when compared to long tone actuation methods.

Original languageEnglish (US)
Title of host publicationAmerican Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013
PublisherAmerican Helicopter Society International
Pages376-384
Number of pages9
ISBN (Print)9781632662828
StatePublished - 2013
Event2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013 - Tianjin, China
Duration: Sep 8 2013Sep 11 2013

Publication series

NameAmerican Helicopter Society International - 2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013

Other

Other2nd Asian/Australian Rotorcraft Forum, ARF 2013 and the 4th International Basic Research Conference on Rotorcraft Technology 2013, IBRCRT 2013
Country/TerritoryChina
CityTianjin
Period9/8/139/11/13

All Science Journal Classification (ASJC) codes

  • Automotive Engineering

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