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

Description
Item Description:	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."
Physical Description:	1 online resource (7 pages) : color illustrations.
Bibliography:	Includes bibliographical references (page 7).