Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / / Ali A. Ameri

• Autore: Ameri Ali A.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
• Descrizione fisica: 1 online resource (25 pages) : illustrations
• Soggetto topico: Computational fluid dynamics; Turbulent boundary layer; Turbine blades; Heat transfer; Losses; Low Reynolds number; Pressure ratio; Three dimensional flow; Laminar flow
• Note generali: Title from title screen (viewed Jan. 15, 2013).; "April 2012."; "This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
• Nota di bibliografia: Includes bibliographical references (pages 24-25).
• Titolo autorizzato: Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910702113803321
• Lo trovi qui: Univ. Federico II