The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / / Christopher E. Hughes [and three others]

• Record Nr.: UNINA9910702436703321
• Autore: Hughes Christopher E.
• Pubbl/distr/stampa: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
• Descrizione fisica: 1 online resource (35 pages) : illustrations (some color)
• Collana: NASA/TM ; ; 2013-214029
• Soggetti: Aeroacoustics; Aerodynamic characteristics; Aerodynamic noise; Aircraft noise; Fan blades; Far fields; Laser doppler velocimeters; Low speed wind tunnels
• Lingua di pubblicazione: Inglese
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Note generali: Title from title screen (viewed July 9, 2014).; "December 2013."; "GT2005-68573."
• Nota di bibliografia: Includes bibliographical references (page 13).