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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 |