Optical characterization of a multipoint lean direct injector for gas turbine combustors [[electronic resource] ] : velocity and fuel drop size measurements / / Christopher M. Heath ... [and others] ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010

• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
• Descrizione fisica: 1 online resource (13 pages) : illustrations, color
• Soggetto topico: Fuel injection; Gas turbines; Flight conditions; Computational fluid dynamics; Combustion chambers; Aircraft engines; Flame temperature; Inlet temperature; Supersonic flight
• Altri autori: HeathChristopher M
• Note generali: Title from title screen (viewed on April 21, 2011).; "October 2010."
• Nota di bibliografia: Includes bibliographical references (page 13).
• Altri titoli varianti: Optical characterization of a multipoint lean direct injector for gas turbine combustors
• Titolo autorizzato: Optical characterization of a multipoint lean direct injector for gas turbine combustors
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910699918403321
• Lo trovi qui: Univ. Federico II