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The static and forward speed testing of a flapped wing with boundary layer control for use in deflecting propeller slipstreams downward for vertical take-off: Part II, tests at incidence and ground proximity effects

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council Canada
FormatText, Technical Report
Physical description1 v.
Publication date
PublisherNational Research Council Canada. National Aeronautical Establishment
Access condition
  • Print copy held at NRC. Digital version available upon request. Contact NRC.NSL-BSN.CNRC@nrc-cnrc.gc.ca
Series
  • Aeronautical Report (National Research Council Canada. National Aeronautical Establishment), no. LR-383.
LanguageEnglish
Peer reviewedNo
NRC numberNRC 7558
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Record identifier01b2af53-bae8-425f-a792-522b7ef24678
Record created2020-02-13
Record modified2025-12-05
Date modified: