Three-dimensional vortex wake structure of a flapping-wing micro aerial vehicle in forward flight configuration

Research output: Contribution to journalArticleScientificpeer-review

19 Citations (Scopus)
Original languageEnglish
Pages (from-to)1-16
Number of pages16
JournalExperiments in Fluids: experimental methods and their applications to fluid flow
Volume55
Issue number9, art.nr. 1806
DOIs
Publication statusPublished - 2014

Keywords

  • CWTS 0.75 <= JFIS < 2.00

Cite this