The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct
By: Milo D. Dahl.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107358.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Supersonic jet flow; Ducts; Ducted flow; Duct geometry; Circles (Geometry); Boundary conditions; Kelvin-Helmholtz instability; Supersonic inlets
Notes: Shipping list no.: 98-0783-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.