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Record Nr. |
UNINA9910700138803321 |
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Autore |
Suder Kenneth L (Kenneth Lee) |
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Titolo |
Results of an advanced fan stage operating over a wide range of speed and bypass ratio / / Kenneth L. Suder [and five others] |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]-[2011] |
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Descrizione fisica |
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1 online resource (2 volumes) : color illustrations |
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Collana |
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NASA/TM ; ; 2010-216769, 2011-216769 |
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Soggetti |
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Aerodynamic stalling |
Bypass ratio |
Computational fluid dynamics |
Propulsion system configurations |
Transonic compressors |
Turbofans |
Supersonic speed |
Computerized simulation |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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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." |
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Nota di bibliografia |
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Includes bibliographical references. |
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Nota di contenuto |
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pt. 1. Fan stage design and experimental results -- pt 2. Comparison of CFD and experimental results. |
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