The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct



Publisher: National Aeronautics and Space Administration, Publisher: National Technical Information Service, distributor in [Washington, D.C, Springfield, Va

Written in English
Published: Downloads: 710
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Subjects:

  • Supersonic jet flow.,
  • Ducts.,
  • Ducted flow.,
  • Duct geometry.,
  • Circles (Geometry),
  • Boundary conditions.,
  • Kelvin-Helmholtz instability.,
  • Supersonic inlets.

Edition Notes

StatementMilo D. Dahl.
SeriesNASA technical memorandum -- 107358.
ContributionsUnited States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL18118420M

The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct Download PDF EPUB FB2