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 |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
Descrizione fisica | 1 online resource (13 pages) : illustrations, color |
Altri autori (Persone) | HeathChristopher M |
Collana | NASA/TM |
Soggetto topico |
Fuel injection
Gas turbines Flight conditions Computational fluid dynamics Combustion chambers Aircraft engines Flame temperature Inlet temperature Supersonic flight |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Altri titoli varianti | Optical characterization of a multipoint lean direct injector for gas turbine combustors |
Record Nr. | UNINA-9910699918403321 |
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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Temperature and species measurements of combustion produced by a 9-point lean direct injector / / Sarah A. Tedder and Yolanda R. Hicks, Randy J. Locke |
Autore | Tedder Sarah A. |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
Descrizione fisica | 1 online resource (15 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Stirling cycle
Carbon dioxide Injectors Raman spectra Nitrogen Flame temperature JP-8 jet fuel |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910704911003321 |
Tedder Sarah A. | ||
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
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