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

Description
Item Description:	Title from title screen (viewed Aug. 2, 2016). "November 1996"--Report documentation page. "Prepared for the International Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996." "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Physical Description:	1 online resource (21 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 11-12).