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Record Nr. |
UNINA9910704241203321 |
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Autore |
Berdanier Reid A. |
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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 |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 |
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Descrizione fisica |
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1 online resource (xiv, 145 pages) : color illustrations |
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Collana |
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Soggetti |
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Wall flow |
Turbocompressors |
Flow visualization |
Leakage |
Turbomachinery |
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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 Feb. 10, 2016). |
"September 2015." |
"Prepared under contract NNX11AI59A." |
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Nota di bibliografia |
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Includes bibliographical references (pages 141-145). |
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