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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



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Autore: Berdanier Reid A. Visualizza persona
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 Visualizza cluster
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  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910704241203321
Lo trovi qui: Univ. Federico II
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