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Autore: | Berdanier Reid A. |
Titolo: | An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / / Reid A. Berdanier and Nicole L. Key |
Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 |
Descrizione fisica: | 1 online resource (xiv, 145 pages) : color illustrations |
Soggetto topico: | Wall flow |
Turbocompressors | |
Flow visualization | |
Leakage | |
Turbomachinery | |
Persona (resp. second.): | KeyNicole L. |
Note generali: | Title from title screen (viewed Feb. 10, 2016). |
"September 2015." | |
"Prepared under contract NNX11AI59A." | |
Nota di bibliografia: | Includes bibliographical references (pages 141-145). |
Titolo autorizzato: | An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor |
Formato: | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910704241203321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |