Investigation of Inlet Distortion on the Flutter Stability of a Highly Loaded Transonic Fan Rotor

Research output: Contribution to book/Conference proceedings/Anthology/ReportConference contributionContributedpeer-review

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Details

Original languageEnglish
Title of host publicationASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
Number of pages11
Publication statusPublished - 20 Sept 2016
Peer-reviewedYes