Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / / Zhuohui J. He [and four others]

• Autore: He Zhuohui J.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014
• Descrizione fisica: 1 online resource (7 pages) : color illustrations
• Soggetto topico: Combustion chambers; Inlet pressure; Inlet temperature; Fuel injection; Combustion temperature; Nitrogen oxides
• Note generali: Title from title screen (viewed on March 25, 2015).; "April 2014."; "Prepared for the 8th U.S. National Combustion Meeting sponsored by the Western State Section, Combustion Institute, Park City, Utah, May 19-22, 2013."
• Nota di bibliografia: Includes bibliographical references (page 7).
• Titolo autorizzato: Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910702438303321
• Lo trovi qui: Univ. Federico II