Results of an advanced fan stage operating over a wide range of speed and bypass ratio / / Kenneth L. Suder [and five others]

• Autore: Suder Kenneth L (Kenneth Lee)
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]-[2011]
• Descrizione fisica: 1 online resource (2 volumes) : color illustrations
• Soggetto topico: Aerodynamic stalling; Bypass ratio; Computational fluid dynamics; Propulsion system configurations; Transonic compressors; Turbofans; Supersonic speed; Computerized simulation
• Note generali: Title from title screen (viewed on Jan. 29, 2014).; "Prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010."
• Nota di bibliografia: Includes bibliographical references.
• Nota di contenuto: pt. 1. Fan stage design and experimental results -- pt 2. Comparison of CFD and experimental results.
• Titolo autorizzato: Results of an advanced fan stage operating over a wide range of speed and bypass ratio
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910700138803321
• Lo trovi qui: Univ. Federico II