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Record Nr. |
UNINA9910703786003321 |
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Autore |
Ibrahim Mounir B. |
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Titolo |
Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2014 |
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Descrizione fisica |
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1 online resource (19 pages) : color illustrations |
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Collana |
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Soggetti |
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Computational fluid dynamics |
Turbine blades |
Rotor blades (turbomachinery) |
Hole distribution (mechanics) |
Hole geometry (mechanics) |
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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 Aug. 7, 2015). |
"November 2014." |
"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014." |
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Nota di bibliografia |
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Includes bibliographical references (page 19). |
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