Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector /

Bibliographic Details

Main Author:	He, Zhuohui J. (Author)
Corporate Author:	Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
Series:	NASA technical memorandum ; 2014-218117.
Subjects:	Combustion chambers. Inlet pressure. Inlet temperature. Fuel injection. Combustion temperature. Nitrogen oxides.
Online Access:	https://purl.fdlp.gov/GPO/gpo54279 http://purl.fdlp.gov/GPO/gpo54279