Last edited by Voodoolrajas
Wednesday, July 8, 2020 | History

2 edition of Blade-mounted flap control for BVI noise reduction proof-of-concept test found in the catalog.

Blade-mounted flap control for BVI noise reduction proof-of-concept test

Blade-mounted flap control for BVI noise reduction proof-of-concept test

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  • 29 Currently reading

Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Blade-vortex interaction.,
  • Wind tunnel tests.,
  • Noise reduction.,
  • Aircraft control.,
  • Flaps (Control surfaces),
  • Helicopters.,
  • Aeroacoustics.,
  • Pressure distribution.,
  • Active control.,
  • Interactional aerodynamics.

  • Edition Notes

    Other titlesBlade mounted flap control for BVI noise reduction proof-of-concept test.
    StatementSeth Dawson ... [et al].
    SeriesNASA contractor report -- 195078., NASA contractor report -- NASA CR-195078.
    ContributionsDawson, Seth., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15504798M


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Blade-mounted flap control for BVI noise reduction proof-of-concept test Download PDF EPUB FB2

Get this from a library. Blade-mounted flap control for BVI noise reduction proof-of-concept test. [Seth Dawson; Langley Research Center.;]. Blade-mounted flap control for BVI noise reduction proof-of-concept test [microform] [] Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va.: National Technical Information Service, distributor, ].

Full text of "NASA Technical Reports Server (NTRS) NASA/Army Rotorcraft 1: Aerodynamics, and Dynamics and Aeroelasticity" See other formats. Full text of "NASA Technical Reports Server (NTRS) Research and technology, " See other formats.

On the generation of side-edge flap noise.[part span trailing edge flaps. NASA Technical Reports Server (NTRS) Howe, M. A theory is proposed for estimating the noise generated at the side edges of part span trailing edge flaps in terms of pressure fluctuations measured just in-board of the side edge of the upper surface of the otic formulae are developed.

Proof of concept testing report. DOT National Transportation Integrated Search. This report documents the methodology and results of. Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A continuing bibliography with indexes (supplement )" See other formats.