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The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley



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Autore: Bozak Richard F. Visualizza persona
Titolo: The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Descrizione fisica: 1 online resource (8 pages) : illustrations (some color)
Soggetto topico: Acoustic properties
Aerodynamic noise
Blade tips
Oscillating flow
Pressure ratio
Turbofans
Rotors
Persona (resp. second.): HughesChristopher E.
BuckleyJames (Mechanical engineer)
Note generali: Title from title screen (viewed June 4, 2014).
"August 2013."
"Prepared for the Turbo Expo 2013 sponsored by the American Society of Mechanical Engineers (ASME) San Antonio, Texas, June 3-7, 2013."
"GT2013-95114."
Nota di bibliografia: Includes bibliographical references (pages 7-8).
Titolo autorizzato: The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910705296503321
Lo trovi qui: Univ. Federico II
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