Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
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Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions semi-annual report to NASA Langley for worked performed under the grant by

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English

Subjects:

  • Blade slap noise.,
  • Blade-vortex interaction.,
  • Helicopters.,
  • Noise prediction.,
  • Rotary wings.,
  • Wind tunnel tests.

Book details:

Edition Notes

Statementprincipal investigators: William J. Devenport, Stewart A.L. Glegg.
SeriesNASA contractor report -- NASA CR-198590.
ContributionsGlegg, Stewart A. L., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15413882M

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