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

• Autore: Dahl Milo D. <1956->
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , November 1996
• Descrizione fisica: 1 online resource (21 pages) : illustrations
• Soggetto topico: Supersonic jet flow; Ducts; Ducted flow; Duct geometry; Circles (geometry); Boundary conditions; Kelvin-Helmholtz instability; Supersonic inlets
• Note generali: 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.
• Nota di bibliografia: Includes bibliographical references (pages 11-12).
• Titolo autorizzato: The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707311303321
• Lo trovi qui: Univ. Federico II