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Advanced propulsion collision damage due to unmanned aerial system ingestion

  • Virginia Polytechnic Institute and State University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

6 Scopus citations

Abstract

An explicit numerical analysis was employed to assess the dynamic damage development in advanced high-bypass propulsion system in the event of a drone ingestion. CFRP was implemented in the fan blade design and rate-dependent metal alloy properties were considered. Details of damage history on the subjected propulsion system were discussed.

Original languageEnglish
Title of host publication30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
PublisherInternational Council of the Aeronautical Sciences
ISBN (Electronic)9783932182853
StatePublished - 2016
Event30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016 - Daejeon, Korea, Republic of
Duration: Sep 25 2016Sep 30 2016

Publication series

Name30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016

Conference

Conference30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
Country/TerritoryKorea, Republic of
CityDaejeon
Period09/25/1609/30/16

Keywords

  • Comprehensive modeling
  • Finite element
  • Foreign object ingestion
  • Propulsion
  • Unmanned aerial system

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