Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine / / by Hugh A. Klassen
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| Autore: |
Klassen Hugh A.
|
| Titolo: |
Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine / / by Hugh A. Klassen
|
| Pubblicazione: | Washington, D.C. : , : National Aeronautics and Space Administration, , August 1968 |
| Descrizione fisica: | 1 online resource (19 pages) : illustrations |
| Soggetto topico: | Turbines - Blades - Testing |
| Turbines - Design and construction | |
| Note generali: | "August 1968." |
| Nota di bibliografia: | Includes bibliographical references (page 19). |
| Titolo autorizzato: | Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910715197003321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |