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: 1996 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
| Statement | Milo D. Dahl. |
| Series | NASA technical memorandum -- 107358. |
| Contributions | United States. National Aeronautics and Space Administration. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL18118420M |
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