Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga

• Record Nr.: UNINA9910702436203321
• Autore: Hughes Christopher E.
• Pubbl/distr/stampa: Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013
• Descrizione fisica: 1 online resource (22 pages) : color illustrations
• Collana: NASA/TM ; ; 2013-216073
• Soggetti: Aircraft performance; Bypass ratio; Fan blades; Fixed wings; Low speed wind tunnels; Noise reduction
• Lingua di pubblicazione: Inglese
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Note generali: Title from title screen (viewed July 9, 2014).; "November 2013."
• Nota di bibliografia: Includes bibliographical references (pages 5-6).