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

Bibliographic Details

Main Author:	Dahl, Milo D., 1956- (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
Series:	NASA technical memorandum ; 107358.
Subjects:	Supersonic jet flow. Ducts. Ducted flow. Duct geometry. Circles (geometry) Boundary conditions. Kelvin-Helmholtz instability. Supersonic inlets.
Online Access:	https://purl.fdlp.gov/GPO/gpo70672