Design and numerical investigation of swirl recovery vanes for the Fokker 29 propeller

Research output: Contribution to journalArticleScientificpeer-review

16 Citations (Scopus)
Original languageEnglish
Pages (from-to)1128-1136
Number of pages9
JournalChinese Journal of Aeronautics
Volume27
Issue number5
DOIs
Publication statusPublished - 2014

Keywords

  • CWTS JFIS < 0.75

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