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Record Nr. |
UNINA9910707311303321 |
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Autore |
Dahl Milo D. <1956-> |
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Titolo |
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / / Milo D. Dahl |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996 |
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Descrizione fisica |
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1 online resource (21 pages) : illustrations |
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Collana |
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NASA technical memorandum ; ; 107358 |
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Soggetti |
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Supersonic jet flow |
Ducts |
Ducted flow |
Duct geometry |
Circles (geometry) |
Boundary conditions |
Kelvin-Helmholtz instability |
Supersonic inlets |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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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. |
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Nota di bibliografia |
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Includes bibliographical references (pages 11-12). |
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